1953...29.5: Cambridge work*
PRESTON, J.H.*
The determination of turbulent skin friction by means of pitot tubes*
J. Roy. Aero. Soc. 58, 109*
1954 .`
..29.2: overestimate asymptotes to about 3 times wall stress at hole size of 600 wall units*
SHAW, R.*
The influence of hole dimensions on static pressure measurements*
J. Fluid Mech. 7, 550*
1960 .`
..29.6,25.1: rigorous definitions*
STUART, J.T.; PANKHURST, R.C.; BRYER, D.W.*
Particle paths, filament lines and streamlines*
Nat. Phys. Lab. Aero Rept 1057*
1963. `
..29.1,30.1: mainly probes and manometers*
ANON.*
Flow measurement facilities and auxiliary equipment*
AVA and MPI fur Stromungsforschung, Gottingen*
1964. `
..29.3: very general case*
BERGH, H.; TIJDEMAN, H.*
Theoretical and experimental results for the dynamic response of prsssure measuring systems*
NLR, Amsterdam, TR F.238*
1965. `
..29.2: large (compared to displacement thickness) holes in compressible flow have errors "many times" Shaw (1960)*
RAINBIRD, W.J.*
Errors in measurement of mean static pressure of a moving fluid due to pressure holes*
Canadian DME/NAE Quart. Bull., pt. 3
1967. `
..29.5: single pivot to one side of element - element stays flush with surface and there is a "mechanical advantage"*
HEADLEY, J.W.*
Skin friction balance*
J. Sci. Instrum. (J. Phys. E), ser. 2 - 2, 380*
1969. `
..29.2: laminar flow expts, calcs and limited measurements in turbulent flow*
BECKER, H.A.; BROWN, A.P.G.*
Response of Pitot probes in turbulent streams*
J. Fluid Mech. 62, 85*
1974. `
..29.6,11.6: quoted by Dahm Phys. Fluids A3, 1115, 1991*
SHERWOOD, T.K.; PIGFORD, R.L.; WILKE, C.R.*
Mass Transfer*
McGraw-Hill*
1975. `
..29.2: corrections*
LAWN, C.J.*
The calibration of a cylindrical pressure probe for recirculating flow measurements*
Berkeley Nuclear Labs., Central Elec. Gen. Board, RD/B/N3269*
1975. `
..29.5,07.0: comments on unreliability of sublayer meas. - see McEligot 1984 draft*
PIERCE, F.J.; GOLD, D.S.*
Near wall velocity measurements for wall shear inference in turbulent flows*
NBS Special Pub. 484, p. 621*
1977. `
..29.6: smoke wire - PB has*
AUTHOR*
A new technique for introducing controlled sheets of smoke streamlines in wind tunnels*
ICIASF Record, p. 74*
1977. `
..29.6:ARL*
POLLOCK, N.*
A simple laser interferometer for wind tunnel flow visualization.*
J. Phys. E, 13, 1062*
1980. `
..29.5: balance gaps filled with liquid*
THOMANN, H.; FREI, D.*
Direct measurements of skin friction in a turbulent boundary layer with a strong adverse pressure gradient.*
J. Fluid Mech. 101, 79*
1980. `
..29.5: sharp lipped*
ALLEN, J. M.*
Improved sensing element for skin-friction balance measurements.*
AIAA J. 18, 1342*
1980. `
..29.6: the coloured light man*
CROWDER, J.P.*
Add fluorescent minitufts to the aerodynamicist's bag of tricks.*
Astro and Aero. Vol. 18, no. 11, p. 54*
1980. `
..29.3:*
WELSH, B.L.; PYNE, C.R.*
A method to improve the temperature stability of semiconductor strain gauge transducers.*
J. Phys. E. 13, 816*
1980. `
..29.1:*
WELSH, B.L.*
An angular displacement transducer.*
J. Phys. E. 13, 826*
1980. `
..01.1,01.2,29.6,31.1:*
FALCO, R.E.*
Combined simultaneous flow visualisation hot-wire anemometry for the study of turbulent flows.*
J. Fluids Engg 102, 174*
1980. `
..29.2:freq. response up to 3kHz - water is easier?*
MURAI, H.; IHARA, A.*
A handy method for measuring turbulence in water by total probes*
Rep. Inst. High Speed Mech., Tohoku Univ., 41, 37*
1980. `
..29.5: floating elt with two eddy current disp. meters*
TENNANT, M.H.; PIERCE, F.J.; McALLISTER, J.E.*
An omnidirectional wall shear meter*
J. Fluids Engg 102, 21*
1980. `
..29.5: cross Stanton tube*
PONTIKOS, N.; BRADSHAW, P.*
Miniature pressure probe for measuring the surface-shear-stress vector in turbulent flow*
Aero. Quart. 32, 43*
1981. `
..29.6: misc - spheres etc*
WERLE, H.*
Transition and separation - visualizations in the ONERA water tunnel*
Rech. Aero. 1980 - 5, p.35*
1981. `
..29.2: just so - and the same to you*
MANUEL, T.*
Automating orifices from top to bottom.*
Electronics 54, 5, 157 (March 10)*
1981. `
..29.6:pulsed smoke wire, .09 mm dia., 37 ms cycle, motorized oil sponge*
KAWAI, S.*
Visualization of airflow separation over wind-wave crests under moderate wind*
Boundary-Layer Met. 21, 93*
1981. `
..29.2: 3rd yr project*
CHRISTIANSEN, T.; BRADSHAW, P.*
Effect of turbulence on pressure probes*
J. Phys. E - Sci. Instrum. 14, 992*
1981. `
..29.6:can match refractive index, also electrochromic*
HENDRIKS, F.; AVIRAM, A.*
The use of zinc iodide solutions in flow research*
IBM Watson Center RC 8885*
1981. `
..29.3:cap. type, perforated dielectric helps*
PORTAT, M.; BRUERE, A.; GODEFROY, J.C.; HELIAS, F.*
Measurement possibilities on turbomachines with thin film transducers*
ONERA TP 1981-103*
1981. `
..29.5:surprisingly large Stanton / Preston diffs - step and rough change*
KISKE, S.; VASANTA RAM, V.; PFARR, K.*
The effect of disturbed turbulence structure on the Preston tube method of measuring wall shear stress*
Aero. Quart. 32, 354*
1981. `
..29.6,29.1:Schlieren with concentric rings instead of knife edge*
OHNDER OZBELGE, H.; LIGHTFOOT, E.N.; MILLER, E.E.*
Reflectance-Schlieren technique for measurement of free liquid surface perturbations*
J.Phys. E. 14, 1381*
1981. `
..29.5: pulsed wall probe - quantitative thermal tuft*
WESTPHAL, R.V.; EATON, J.K.; JOHNSTON, J.P.*
A new probe for measurement of velocity and wall shear stress in unsteady reversing flow*
J. Fluids Engg 103, 478*
1981. `
..29.5:see also Poll CoA 8308*
REED, T.D.; ABU-MOSTAFA, A.; STEINLE, F.S.*
Correlation of Preston tube data with laminar skin friction*
AIAA J. 21, 379*
1983. `
..05.0,01.1,29.6: which comes first, streak or burst*
SMITH, C.R.; METZLER, S.P.*
The characteristics of low speed streaks in the near wall region of a turbulent boundary layer*
J. Fluid Mech. 129, 27*
1983. `
..29.4,42.3: measure inversion height below solid roof*
BAINES, W.D.*
A technique for the direct measurement of volume flux of a plume*
J. Fluid Mech. 132, 247*
1983. `
..17.2,29.6:l.e. vortices shown beautifully*
FREYMUTH, P.; BANK, W.; PALMER, M.*
Use of Titanium Tetrachloride for visualization of accelerating flow around airfoils*
Proc. 3rd Int. Symp. on Flow Viz., Ann Arbor and Z. Flug. und Welt. (ZFW) 7, 392*
1983. `
..29.2: Siddon type strain gauged wing*
WHITE, A.S.; PARKER, A.G.*
A yawmeter for steady and low frequency unsteady flows*
J. Phys. E., Sci. Instrum. 16, 231*
1983. `
..29.6:ICI Waxoline powder dye and oil on smoke wire*
SIEVERDING, C.H.; VAN DEN BOSCHE, P.*
The use of coloured smoke to visualize secondary flows in a turbine blade cascade*
J. Fluid Mech. 134, 85*
1983. `
..29.4:poop, poop -adj. time delay for coincidence at downstream mark*
IRITANI, Y.; KASAGI, N.; HIRATA, M.*
Direct velocity measurement in low speed water flows by double wire hydrogen bubble technique*
Expts. in Fluids 1, 111*
1983. `
..29.2:use P at upwind hole instead of centre one*
OSTOWARI, C.; WENTZ, W.H.*
Modified calibration technique of a five hole probe for high flow angles*
Expts. in Fluids 1, 166*
1983. `
..29.1,31.1:11 chapters inc. 2-ph and non-N*
GOLDSTEIN, R.J. (Ed.)*
Fluid Mechanics Measurements*
Hemisphere/Springer*
1983. `
..05.0,29.6: streaks are active outward motions - contradicts Falco AD-A122 581*
SMITH, C.R.; SCHWARTZ, S.P.*
Observation of streamwise rotation in the near wall region of a turbulent boundary layer*
Phys. Fluids 26, 641*
1983. `
..05.0,29.6: organized but looks chaotic*
CERRA, A.W.; SMITH, C.R.*
Experimental observations of vortex ring interaction with the fluid adjacent to a surface*
Lehigh Univ. M.E. Dept Rept FM-4*
1983. `
..31.1,29.6: the nice unsteady aerofoil pics - see also Ann Arbor*
FREYMUTH, P.; BANK, W.; PALMER, M.*
Flow visualization and hot wire anemometry*
TSI Quart. vol. 9, no. 4, p. 14*
1983. `
..29.1:General chat about B.B.*
ESCUDIER, M.P.*
The instrumentation of a modern fluid mechanics research laboratory*
Measurement and Control 16, 230 and 267*
1983. `
..29.6:axi filter for knife-edge - see also Appl. Optics 23, 2449, 1984*
HOWES, W.D.*
Rainbow Schlieren*
NASA TP 2166*
1983. `
..05.0,29.6: dual view video*
SMITH, C.R.; PAXSON, R.D.*
A technique for evaluation of three dimensional behavior in turbulent boundary layers using computer augmented hydrogen bubble wire flow visualization*
Expts. in Fluids 1, 43*
1983. `
..29.6:smoke and swept 5W laser - conc. assumed same as light intensity*
BALINT, J.L.A.; AYRAULT, M.; SCHON, J.P.*
Quantitative investigation of the velocity and concentration fields of turbululent flows combining visualization and image processing*
Third Int. Symp. on Flow Viz., Ann Arbor*
1983. `
..29.5:continuous expressions for Patel calibn*
POLL, D.I.A.*
Note on the algebraic representation of the Preston tube calibration*
Cranfield College of Aeronautics Rept CAR-8308*
1983. `
..53.0,29.6: dye and bubbles -no T-G vortices*
JEANS, A.J.; JOHNSTON, J.P.*
The effects of concave curvature on turbulent boundary layer structures*
Structure of Complex Turbulent Shear Flow (R. Dumas and L. Fulachier, Eds.) Springer, p. 89*
1983. `
..29.1: DC motor designs - var. speed AC (electronic drive) improving*
BALL, D.A.*
Motors and motor drives - the new challenge*
Electronics and Power 29, 135*
1983. `
..29.5,05.0:includes spectra and scales*
YEFIMTSOV, B.M.; KUZNETSOV, V.B.; SYSOYEV, V.A.*
Turbulent fluctuations of shear stress at the wall*
Fluid Mech. - Soviet Research 12, 121*
1983. `
..29.5: semi-theoretical calibration - the usual variables*
POLL, D.I.A.*
A note on the use of surface pitot tubes for the measurement of skin friction in laminar boundary layers*
Cranfield Coll of Aero Report 8307*
1983. `
..29.5:see also Poll CoA 8308*
REED, T.D.; ABU-MOSTAFA, A.; STEINLE, F.S.*
Correlation of Preston tube data with laminar skin friction*
AIAA J. 21, 379*
1983. `
..05.0,01.1,29.6: which comes first, streak or burst*
SMITH, C.R.; METZLER, S.P.*
The characteristics of low speed streaks in the near wall region of a turbulent boundary layer*
J. Fluid Mech. 129, 27*
1983. `
..29.4,42.3: measure inversion height below solid roof*
BAINES, W.D.*
A technique for the direct measurement of volume flux of a plume*
J. Fluid Mech. 132, 247*
1983. `
..17.2,29.6:l.e. vortices shown beautifully*
FREYMUTH, P.; BANK, W.; PALMER, M.*
Use of Titanium Tetrachloride for visualization of accelerating flow around airfoils*
Proc. 3rd Int. Symp. on Flow Viz., Ann Arbor and Z. Flug. und Welt. (ZFW) 7, 392*
1983. `
..29.2: Siddon type strain gauged wing*
WHITE, A.S.; PARKER, A.G.*
A yawmeter for steady and low frequency unsteady flows*
J. Phys. E., Sci. Instrum. 16, 231*
1983. `
..29.6:ICI Waxoline powder dye and oil on smoke wire*
SIEVERDING, C.H.; VAN DEN BOSCHE, P.*
The use of coloured smoke to visualize secondary flows in a turbine blade cascade*
J. Fluid Mech. 134, 85*
1983. `
..29.4:poop, poop -adj. time delay for coincidence at downstream mark*
IRITANI, Y.; KASAGI, N.; HIRATA, M.*
Direct velocity measurement in low speed water flows by double wire hydrogen bubble technique*
Expts. in Fluids 1, 111*
1983. `
..29.2:use P at upwind hole instead of centre one*
OSTOWARI, C.; WENTZ, W.H.*
Modified calibration technique of a five hole probe for high flow angles*
Expts. in Fluids 1, 166*
1983. `
..29.1,31.1:11 chapters inc. 2-ph and non-N*
GOLDSTEIN, R.J. (Ed.)*
Fluid Mechanics Measurements*
Hemisphere/Springer*
1983. `
..05.0,29.6: streaks are active outward motions - contradicts Falco AD-A122 581*
SMITH, C.R.; SCHWARTZ, S.P.*
Observation of streamwise rotation in the near wall region of a turbulent boundary layer*
Phys. Fluids 26, 641*
1983. `
..05.0,29.6: organized but looks chaotic*
CERRA, A.W.; SMITH, C.R.*
Experimental observations of vortex ring interaction with the fluid adjacent to a surface*
Lehigh Univ. M.E. Dept Rept FM-4*
1983. `
..31.1,29.6: the nice unsteady aerofoil pics - see also Ann Arbor*
FREYMUTH, P.; BANK, W.; PALMER, M.*
Flow visualization and hot wire anemometry*
TSI Quart. vol. 9, no. 4, p. 14*
1983. `
..29.1:General chat about B.B.*
ESCUDIER, M.P.*
The instrumentation of a modern fluid mechanics research laboratory*
Measurement and Control 16, 230 and 267*
1983. `
..29.6:axi filter for knife-edge - see also Appl. Optics 23, 2449, 1984*
HOWES, W.D.*
Rainbow Schlieren*
NASA TP 2166*
1983. `
..05.0,29.6: dual view video*
SMITH, C.R.; PAXSON, R.D.*
A technique for evaluation of three dimensional behavior in turbulent boundary layers using computer augmented hydrogen bubble wire flow visualization*
Expts. in Fluids 1, 43*
1983. `
..29.6:smoke and swept 5W laser - conc. assumed same as light intensity*
BALINT, J.L.A.; AYRAULT, M.; SCHON, J.P.*
Quantitative investigation of the velocity and concentration fields of turbululent flows combining visualization and image processing*
Third Int. Symp. on Flow Viz., Ann Arbor*
1983. `
..29.5:continuous expressions for Patel calibn*
POLL, D.I.A.*
Note on the algebraic representation of the Preston tube calibration*
Cranfield College of Aeronautics Rept CAR-8308*
1983. `
..53.0,29.6: dye and bubbles -no T-G vortices*
JEANS, A.J.; JOHNSTON, J.P.*
The effects of concave curvature on turbulent boundary layer structures*
Structure of Complex Turbulent Shear Flow (R. Dumas and L. Fulachier, Eds.) Springer, p. 89*
1983. `
..29.1: DC motor designs - var. speed AC (electronic drive) improving*
BALL, D.A.*
Motors and motor drives - the new challenge*
Electronics and Power 29, 135*
1983. `
..29.5,05.0:includes spectra and scales*
YEFIMTSOV, B.M.; KUZNETSOV, V.B.; SYSOYEV, V.A.*
Turbulent fluctuations of shear stress at the wall*
Fluid Mech. - Soviet Research 12, 121*
1983. `
..29.5: semi-theoretical calibration - the usual variables*
POLL, D.I.A.*
A note on the use of surface pitot tubes for the measurement of skin friction in laminar boundary layers*
Cranfield Coll of Aero Report 8307*
1983. `
..29.6,59.0:the Kraken's wake*
ILEGBUSI, J.O.; SPALDING, D.B.*
A steady unsteady visualization technique for wake flow studies*
J. Fluid Mech. 139, 435*
1984. `
..29.6:several laser based techniques*
LAUTERBORN, W.; VOGEL, A.*
Modern optical techniques in fluid mechanics*
Ann. Rev. Fluid Mech. 16, 223*
1984. `
..29.6,61.0:driven cavity - even lam. flow can have T-G vortices in corners*
KOSEFF, J.R.; STREET, R.L.*
Visualization studies of a shear driven three dimensional recirculating flow*
J. Fluids Engg 106, 21*
1984. `
..29.6,61.0:nice flow viz of sphere vortex street*
MODI, V.J.; AKUTSU, T.*
Wall confinement effects for spheres in the Reynolds number range of 30 - 2000*
J. Fluids Engg 106, 66*
1984. `
..29.6: two meas for vector - mentions Tanner this time*
MONSON, D.J.*
A laser interferometer for measuring skin friction in three dimensional flows*
AIAA J. 22, 557*
1984. `
..29.2:conventional 5 tube yawmeter*
SAMET, M.; EINAV, S.*
Directional pressure probe*
Rev. Sci. Instrum. 55, 582*
1984. `
..29.6: Schlieren - heat jet to ambient density for bigger drho/dy*
HSIA, Y.; BAGANOFF, D.; KROTHAPALLI, A.; KARAMCHETI, K.*
An enhanced flow visualization technique for planar free shear layers*
AIAA J. 22, 439*
1984. `
..29.2: seems to have got all the dim. analysis wrong*
DUCRUET, C.; DYMENT, A.*
The pressure hole problem*
J. Fluid Mech. 142, 251*
1984. `
..29.5:new analytic fit to P-tube cal - from liquid sealed floating elt*
ZURFLUH, U.E.*
Experimental determination of surface shear stress in turbulent boundary layers*
Diss. ETH No. 7528, see Hirt no. 7531*
1984. `
..29.5: pos. or neg. P-tube errors in non eqm flows*
HIRT, F.*
Readings of a Preston tube in a pressure gradient*
Diss. ETH No. 7531, see Zurfluh no. 7528*
1984. `
..29.5: cavity below fibre film - surely recirc ruins freq response*
HOUDEVILLE, H.; JUILLEN, J.C.; COUSTEIX, J.*
Skin friction measurement using hot element gauges*
Rech. Aero. 1984 no. 1, p. 67*
1984. `
..29.6:useful intro - 40 refs*
MANNAN, Z.*
Flow visualization at low speeds*
MSc Essay, Imperial College*
1984. `
..17.2,29.6: better repro. in Amer. Scientist 72,242*
PALMER, M.; FREYMUTH, P.*
Analysis of vortex development from visualizations of accelerating flow around an airfoil, starting from rest*
AIAA-84-1568*
1984. `
..56.0,29.6:pub. version of Marseille paper*
WEI, Q.D.; SATO, H.*
An experimental study of the mechanism of intermittent separation of a turbulent boundary layer*
J. Fluid Mech. 143, 153*
1984. `
..29.6: just so - see NASA TP 2166*
HOWES, W.D.*
Rainbow Schlieren and its application*
Applied Optics 23, 2449*
1984. `
..29.6: vidicon 4Kx4K, finite impulse response filters*
CORKE, T.C.*
Digital image filtering in visualized bondary layers*
AIAA J. 22, 1124*
1984. `
..29.6,28.3: digitizing appears to be manual*
UTAMI, T.; UENO, T.*
Visualization and picture processing of turbulent flow*
Expts. in Fluids 2, 25*
1984. `
..29.2: apparently pub. version of a paper referrred to by Zilliac*
GERNER, A.A.; MAURER, C.L.; GALLINGTON, R.W.*
Non-nulling seven-hole probes for high angle flow measurement*
Expts. in Fluids 2, 93*
1984. `
..29.3: coloured lights again*
SAVORY, E.; TOY, N.*
A technique for visualising the flow field associated with surface-mounted models*
Expts. in Fluids 2, 165*
1984. `
..29.6: two strobe slits, short or long*
HAMPSHIRE, R.G.*
Flow visualization with stroboscopic illumination to provide an unambiguous record of direction*
J. Phys. E. 17, 741*
1984. `
..29.5,59.0:pulsed wall gauge - near wake mixing little changed by vortices*
HUNT, A.; CASTRO, I.P.*
Fluctuating surface shear stresses on bluff bodies*
J. Wind Engg Indust. Aero. 17, 133*
1984. `
..29.5,05.0: wire near wall - zero crossings*
BADRINARAYANAN, M.A.; RAGHU, S.; PODDAR, K.*
Wall shear fluctuations in a turbulent boundary layer*
AIAA J. 22, 1336*
1984. `
..29.6: useful review*
BAXTER, D.R.J.*
Some methods of jet flow visualization and associated photographic techniques*
J. of Photo. Sci. 32, 189*
1984. `
..29.6,25.5: vast effects of ribs on downstream side of cavity*
KENN, M.J.*
Flow visualization aids cavitation studies*
IAHR Symposium on Scale Effects, Esslingen*
1984. `
..29.5:semi theoretical dynamic response eqn*
MENENDEZ, A.N.; RAMAPRIAN, B.R.*
Measurement of skin friction in unsteady boundary layers using a flush mounted hot film gauge*
Iowa Inst of Hydr. Res. IIHR-272*
1984. `
..29.6: Ames - usual plus LIF*
STAFF, Aero. Res. Branch*
A collection of flow visualization techniques used in the Aerodyamics Research Branch*
NASA TM 85998*
1984. `
..05.0,29.6: produced by hemisphere*
ACARLAR, M.S.; SMITH, C.R.*
An experimental study of hairpin-type vortices as a potential flow structure of turbulent boundary layers*
Lehigh Univ. Report FM-5*
1984. `
..29.6: re-inventing*
MOIR, I.R.M.*
Recent experience in the RAE 5 metre wind tunnel of a china clay method for indicating boundary layer transition*
RAE TM AERO 2007 - see also Aero. J. 90, 6, 1986*
1984. `
..02.2,29.6:LDV and smoke to track interface*
CHEVRAY, R.*
Entrainment in turbulent flows - mechanisms and implications*
Turbulence and Chaotic Phenomena in Fluids (T. Tatsumi, Ed.) North-Holland, p.365*
1984. `
..01.2,29.6:multi smoke wire, Rtheta=940*
WEI, W.D.; SAITO, H.; ONDA, Y.*
The visualized large-scale motions in the turbulent boundary layer*
Turbulence and Chaotic Phenomena in Fluids (T. Tatsumi, Ed.) North-Holland, p.391*
1984. `
..02.2,29.6:Head-like, enhanced by diagonal differentiation*
WALLACE, J.M.*
Observations on the nature and mechanism of the bounded turbulent shear flow structure*
Turbulence and Chaotic Phenomena in Fluids (T. Tatsumi, Ed.) North-Holland, p.447*
1984. `
..29.5,31.1: uses Huffman sublayer profile*
McELIGOT, D.M.*
Measurement of wall shear stress in accelerating turbulent flows*
Max-Planck-Inst. Bericht 109*
1984. `
..01.1,29.6: clear insight into unsteady smoke plumes and selective conditional sampling*
SATO, H.*
Cognition and description of patterns in turbulent flows*
Proc 2nd Asian Congr. Fluid Mech. (T.C. Lin, H. Sato and R. Narasimha, Eds.) VNU Science Press, Utrecht, p. 7*
1984. `
..24.1,29.6: NH3 and HCl*
CHEVRAY, R.; SHERIKAR, S.V.*
Entrainment in coherent structures*
Proc 2nd Asian Congr. Fluid Mech. (T.C. Lin, H. Sato and R. Narasimha, Eds.) VNU Science Press, Utrecht, p. 129*
1984. `
..48.0,29.6: just so*
SAVILL, A.M.; ZHOU, M.D.*
Wake/boundary layer and wake-wake interactions - smoke flow visualisation and modelling*
Proc 2nd Asian Congr. Fluid Mech. (T.C. Lin, H. Sato and R. Narasimha, Eds.) VNU Science Press, Utrecht, p. 743*
1984. `
..29.5: urtext IJHMT 17, 1151, 1974 - McLeod*
SALUJA, C.L.; LAMPARD, D.; HAY, N.; BURNS, I.*
The determination of heat transfer coefficients on film cooled flat surfaces using the swollen polymer technique*
Some Chem Engg conference, date approx*
1984. `
..29.5,32.1: fringe fan*
NAQWI, A.A.; REYNOLDS, W.C.; CARR, L.W.*
Dual cylindrical wave laser-doppler method for measurement of wall shear stress*
Laser Anemometry in Fluid Mechanics, p.105, Ladoan / Inst. Superior Tecnico, Lisbon*
1984. `
..61.0,29.6: owl-faces etc*
BIPPES, H.; TURK, M.*
Oil flow patterns of separated flow on a hemisphere cylinder at incidence*
DFVLR-FB 84-20*
1984. `
..29.6,45.0: techniques - mainly laser light plane*
NELSON, R.C.*
Flow visualization of high angle of attack vortex wake structures (invited paper)*
AIAA-85-0102*
1985. `
..29.6,05.5: LIF in crystals on water surface*
GHARIB, M.; HERNAN, M.A.; YAVROUIAN, A.H.; SAROHIA, V.*
Flow velocity measurement by image processing of optically activated tracers*
AIAA-85-0172 and AGARD CP 413, 1986*
1985. `
..29.5,32.1: Tanner rides again*
MURPHY, J.D.; WESTPHAL, R.V.*
The laser-interferometer skin-friction meter - a numerical and experimental study*
Presented at 3rd Symp. on Num. and Phys. Aspects of Aerod. Flows, Long Beach, p. 7-1 (not in Proc.)*
1985. `
..29.6:pH-sensitive dye combinations*
GARDNER, R.A.*
Colorimetric flow visualization*
Expts. in Fluids 3, 33*
1985. `
..29.6,23.0: LIF for quantitative pressure fluctuation*
ACKERMANN, U.; BAGANOFF, D.; McDANIEL, J.C.*
Dependence of laser-induced fluorescence on gas-dynamic fluctuations with application to measurements in unsteady flows*
Expts. in Fluids 3, 45*
1985. `
..29.6,60.0: mainly Schlieren*
MUELLER, T.J.*
The role of flow visualization in the study of afterbody and base flows. A review*
Expts. in Fluids 3, 61*
1985. `
..29.6: two images and time correlation - part 2 on p. 277*
GRANDKE, T.*
Theory and application of the laser shadow technique. Part 1.*
Expts. in Fluids 3, 77*
1985. `
..29.2: quasi-steady theory and some meas.*
CHO, S.H.; BECKER, H.A.*
Response of static pressure probes in turbulent streams*
Expts. in Fluids 3, 93*
1985. `
..29.6: align with stream surfaces but then flip*
SAVAS, O.*
On flow visualization using reflective flakes*
J. Fluid Mech. 152, 235*
1985. `
..29.5: just so - Brown, Boveri work.*
ACHARYA, M.; BORNSTEIN, J.; ESCUDIER, M.P.; VOKURKA, V.*
Development of a floating element for the measurement of surface shear stress*
AIAA J. 23, 410*
1985. `
..59.0,29.5,31.1: pulsed wall gauge*
ADAMS, E.W.; JOHNSTON, J.P.*
Effects of the upstream boundary layer thickness and state on the structure of reattaching flows*
Presented at 5th Symposium on Turbulent Shear Flows, Cornell, p. 5-1 (not in Proc.)*
1985. `
..29.6: IC Chem Engg did it before Hampshire 1984*
POPOVICH, M.M.*
Comment on 'Flow visualization with stroboscopic illumination to provide an unambiguous record of direction'*
J. Phys. E 18, 716*
1985. `
..29.2: still shear errors*
SITARAM, N.; TREASTER, A.L.*
A simplified method of using four-hole probes to measure three-dimensional flow fields*
ASME J. Fluids Engg 107, 31*
1985. `
..29.5: like Pontikos but fences only 1 . 4 mm long*
HIGUCHI, H.*
A miniature, directional surface-fence gage*
AIAA J. 23, 1195*
1985. `
..29.5: wire-and-cavity skin friction gauge*
BLANCHARD, A.*
Instrumentation and testing techniques in the T2 transonic cryogenic wind tunnel at the ONERA/CERT*
Presented at llth ICIASF, Stanford, p. 9*
1985. `
..29.6,28.1: parallel architecture*
MORAITIS, C.S.; MAISTROS, J.G.*
A microcomputer system for real time digitized image compression*
Presented at llth ICIASF, Stanford, p. 133*
1985. `
..29.6:admirably detailed instructions - and warnings about drag increments*
DOBNEY, D.G.; HANSON, P.; FIDDES, S.P.*
The "minituft" surface flow visualisation method - experience of use in the RAE 5m pressurised low-speed wind tunnel*
RAE TM Aero 2038 - and Aero. J. 90, 10, 1986*
1985. `
..09.4,05.0,29.6: VITA on wall stress between riblets only - smoke wire too*
CHOI, K.S.*
Near-wall turbulence structure on a riblet wall*
BMT Ltd Paper*
1985. `
..32.2,29.6: for axi. flow - Abel transform for point resolution*
GRANDKE, T.*
Theory and application of the laser shadow technique. Part 2*
Expts. in Fluids 3, 277*
1985. `
..29.6:uses 1kW mercury lamp*
MORRIS, O.A.; CORLETT, W.A.; WASSUM, D.L.; BABB, C.D.*
Vapor screen technique for flow visualization in the Langley unitary plan wind tunnel*
NASA TM 86384*
1985. `
..29.2: straightfoward and useful intro to yawmeters*
WICKENS, R.H.; WILLIAMS, C.D.*
Calibration and use of five-hole flow direction probes for low speed wind tunnel application*
Canadian NAE-AN-29*
1985. `
..29.5,31.1:exhaustive discussion*
MATHEWS, J.; POLL, D.I.A.*
The theory and application of heated films for the measurement of skin friction*
Cranfield CoA Rept 8515*
1985. `
..24.1,29.6: LIF - 3D eddies*
DAHM, W.J.A.*
Experiments on entrainment, mixing and chemical reactions in turbulent jets at large Schmidt number*
PhD thesis, Caltech*
1985. `
..29.6: LIF time-delay interference for secondary flow*
PURNELL, A.F.*
A Moire approach to flow velocimetry*
Presented at Euromech Colloquium 202, "Measurement Techniques in Low Speed Turbulent Flows"*
1985. `
..29.2: 10-hole yaw and pitch probe*
KOHN, A.*
Flow field measurements in the 3-m x 3-m low speed windtunnel of the DFVLR in Gottingen*
DFVLR-Mitt. 85-14*
1985. `
..17.2,29.6: hysteresis loop depending on freq*
GAD-EL-HAK, M.; HO, C.M.*
The pitching delta wing*
AIAA J. 23, 1660*
1985. `
..24.1,29.6: LIF - shows vortex core is fast fluid*
KOOCHESFAHANI, M.M.; DIMOTAKIS, P.E.*
Laser-induced fluorescence measurements of mixed fluid concentration in a liquid plane shear layer*
AIAA J. 23, 1700*
1985. `
..29.6: from APS meeting poster session*
REED, H.L.*
Gallery of Fluid Motion*
Phys. Fluids 28, 2631*
1985. `
..29.6: vorton model based on Ahlborn method*
AHLBORN, B.; AHLBORN, F.; LOEWEN, S.*
A model for turbulence based on rate equations*
J. Phys. D, Appl. Phys. 18, 2127*
1985. `
..44.2,45.0,29.6: smoke - not directly related to 85-GT-217. VD has*
SONODA, T.*
Experimental investigation on spatial development of streamwise vortices in a turbine inlet guide vane cascade*
ASME paper 85-GT-20*
1985. `
..31.1,29.5: simple unsteady theory*
MENENDEZ, A.N.; RAMAPRIAN, B.R.*
The use of flush-mounted hot-film gauges to measure skin friction in unsteady boundary layers*
J. Fluid Mech. 161, 139*
1985. `
..29.6,59.2: plan view of smoke*
FREYMUTH, P.; FINAISH, F.; BANK, W.*
Three-dimensional vortex patterns in a starting flow*
J. Fluid Mech. 161, 239*
1985. `
..31.3,29.5: liquid crystals*
IRELAND, P.T.; JONES, T.V.*
The measurement of local heat transfer coefficients in blade cooling geometries*
AGARD Conf. Proc. 390*
1985. `
..29.6,61.0: especially noses*
WERLE, H.*
Principaux types de decollement libre observes sur maquettes ellipsoidales*
ONERA Note Tech. 1985-7*
1985. `
..29.6: polyaphrons*
SCHETZ, J.A.*
New flow visualization technique for water tunnel testing of combustors*
AFWAL-TR-85-2042, AD-A158 015*
1985. `
..07.0,29.5 Escudier (1987) non placet, rationem habet*
NITSCHE, W.; THUNKER, R.; HABERLAND, C.*
A computational Preston tube method*
Turbulent Shear Flows 4 - Karlsruhe (L.J.S. Bradbury et al., Eds.). Springer, p.261*
1985. `
..29.5,06.0: details of floating element*
ACHARYA, M.; ESCUDIER, M.P.*
Measurements of the wall shear stress in boundary layer flows*
Turbulent Shear Flows 4 - Karlsruhe (L.J.S. Bradbury et al., Eds.). Springer, p.277 (Proc. p. 176)*
1985. `
..11.4,29.4: spectrometer results from phosphor dots*
NOEL, B.W.; ET AL.*
A proposed method for remote thermometry in turbine engines*
AIAA-85-1468*
1985. `
..29.2: crossflow not bad, incidence awful*
TAMIGNIAUX, T.L.B.; OATES, G.C.*
Effect of a nearby solid surface on a five-hole pressure probe*
AIAA J. 24, 335 (was AIAA-85-0334)*
1986. `
..24.4,29.6: flow viz and wake-like 3D vortices*
BANDYOPADHYAY, P.R.*
Aspects of the equilibrium puff in transitional pipe flow*
J. Fluid Mech. 163, 439*
1986. `
..12.1,29.6: bubbles and LDV, grouped bursts*
TALMON, A.M.; KUNEN, J.M.G.; OOMS, G.*
Simultaneous flow visualization and Reynolds-stress measurement in a turbulent boundary layer*
J. Fluid Mech. 163, 459*
1986. `
..29.5:endless belt instead of surface element - insensitive to p.g.*
VAKILI, A.D.; WU, J.M.; LAWING, P.L.*
Wall shear stress measurements using a new transducer*
AIAA-86-1092*
1986. `
..29.5: automated data reduction*
WESTPHAL, R.V.; BACHALO, W.D.; HOUSER, M.H.*
Improved skin friction interferometer*
NASA-TM-88216*
1986. `
..24.4,29.5,30.2: depend on (unmeasured) free stream turb. - increasing CR delays transition*
KREPLIN, H.P.; MEIER, H.U.; MERCKER, E.; LANDHAUSSER, A.*
Wall shear stress measurements on a prolate spheroid at zero incidence in the DNW wind tunnel*
DFVLR-Mitt. 86-06*
1986. `
..09.1,29.6: 256-diode Reticon camera*
GAD-EL-HAK, M.*
The response of elastic and viscoelastic surfaces to a turbulent boundary layer*
J. Appl. Mech. 53, 206*
1986. `
..45.0,61.0,29.6: fluorescent minitufts - up to four vortices. Names are really WU, WANG and TIAN*
GENXING, W.; TZEHSING, W.; SHIXHONG, T.*
Investigation of vortex patterns on slender bodies at high angles of attack*
J. Aircraft 23, 321*
1986. `
..29.6: tow dye-coated wires through a slightly stable tank before the test*
GAD-EL-HAK, M.*
The use of the dye-layer technique for unsteady flow visualization*
J. Fluids Engg 108, 34*
1986. `
..29.6: laser-based techniques*
BRYANSTON-CROSS, P.J.*
High speed flow visualisation*
Prog. Aerospace Sci. 23, 85*
1986. `
..29.2: d, plus up to 6000 - porous plugs help*
PLENTOVICH, E.B.; GLOSS, B.B.*
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel*
NASA-TP-2545*
1986. `
..05.0,29.6: w from H2 bubble tracking seems large*
KASAGI, N.; HIRATA, M.; NISHINO, K.*
Streamwise pseudo-vortical structures and associated vorticity in the near-wall region of a wall-bounded turbulent shear flow*
Expts. in Fluids 4, 309*
1986. `
..20.0,18.0,29.6: laser planogram*
BONNET, J.P.; CHAPUT, E.*
Large-scale structures visualisation in a high Reynolds number, turbulent flat-plate wake at supersonic speed*
Expts. in Fluids 4, 350*
1986. `
..29.6: general conical laser light sheet - digitally driven mirrors*
PRENEL, J.P.; PORCAR, R.; REINICHE, S.; DIEMUNSCH, G.*
Optical oscilloscope for three-dimensional flow visualization*
Optics and Laser Tech. 18, 208*
1986. `
..29.5: just so*
MURPHY, J.D.; WESTPHAL, R.V.*
The laser interferometer skin-friction meter - a numerical and experimental study*
J. Phys. E - Sci. Instrum, 19, 744*
1986. `
..29.6: emphasis on high speeds but good general review*
SETTLES, G.S.*
Modern developments in flow visualization*
AIAA J. 24, 1313*
1986. `
..29.5: pub version*
HIRT, F.; ZURFLUH, U.; THOMANN, H.*
Skin friction balances for large pressure gradients*
Expts. in Fluids 4, 296*
1986. `
..29.5: Frei, JFM 1980, too optimistic about corrections for Preston tubes*
HIRT, F.; THOMANN, H.*
Measurement of wall shear stress in turbulent boundary layers subject to strong pressure gradients*
J. Fluid Mech. 171, 547*
1986. `
..29.6:aerod. force 1000 times centrifugal force*
O'LEARY, C.O.; DREW, W.*
Flow visualization on rolling models using minitufts*
RAE TM Aero 2083, and Aero. J. 91, 269, 1987*
1986. `
..29.6,28.1: just so*
TOY, N.; WISBY, C.*
A preliminary investigation into the real-time image analysis of a visualized turbulent wake*
Presented at 10th Sympo. on Turbulence, Rolla.*
1986. `
..24.4,29.6:interferometer for fluctuations*
AZZAZY, M.; MODARRESS, D.; TROLINGER, J.D.*
Feasibility study of optical boundary layer transition detection methods*
NASA-CR-178109, N86-28675*
1986. `
..29.5: surface gauges have a phase lag*
GIDDINGS, T.A.; COOK, W.J.*
Response of hot element flush wall gauges in oscillating laminar flow*
NASA-CR-177083, N86-29151*
1986. `
..29.5: Ajagu-like but with sandwiched films*
AOYAGI, M.; TAKEHANA, N.; MASUDA, S.; ARIGA, I.*
Improvement of hot film surface gage for wall shear stress measurement*
Fluid Control and Measurement, vol. 2, p. 863 (M. Harada, Ed.), Pergamon*
1986. `
..29.5: endless belt - does it work? *
VAKILI, A.D.; WU, J.M.*
Direct measurement of skin friction with a new instrument.*
Fluid Control and Measurement, vol. 2, p. 875 (M. Harada, Ed.), Pergamon*
1986. `
..62.0,11.6,29.6: cubic flame holder - nice colour pics*
MURTHY, S.N.B.; WARNER, C.F.; YAN, J.*
Ignition and flame stability of fuel jet through blockers in cross flow*
AIAA-86-1535*
1986. `
..05.0,29.6: 3 components from particles and shifted light sheet*
UTAMI, T.; UENO, T.*
Experimental study on the coherent structure of turbulent open-channel flow using visualization and picture processing*
J. Fluid Mech. 174, 399*
1987. `
..29.5: inclined static pressure holes*
ONSRUD, G.; PERSEN, L.N.; SAETRAN, L.R.*
On the measurement of wall shear stress*
Expts. in Fluids 5, 11*
1987. `
..29.5: disapproves of Nitsche "variable kappa"*
ESCUDIER, M.P.; ACHARYA, M.*
Critique of the computational Preston tube method*
Expts. in Fluids 5, 59*
1987. `
..29.5: not entirely convincing reply to Escudier and Acharya*
NITSCHE, W.*
Rebuttal to "Critique of the computational Preston tube method"*
Expts. in Fluids 5, 63*
1987. `
..29.6: set of 5mW LEDs*
HILLIER, W.; LENT, H.M.; MEIER, G.E.A.; STASICKI, B.*
A pulsed light generator for high speed photography*
Expts. in Fluids 5, 141*
1987. `
..05.0,29.5: VITA averages scaled on inner variables depend weakly on Re*
SHAH, D.A.; ANTONIA, R.A.*
Scaling of wall shear stress fluctuations in a turbulent duct flow*
AIAA J. 25, 22*
1987. `
..29.2: sphere with slots to 112 deg. - 20 mm dia.*
BLACKMORE, P.A.*
A static pressure probe for use in turbulent three-dimensional flows*
J. Wind Engg and Indust. Aero. 25, 207*
1987. `
..11.3,45.0,29.6: nice flow viz. - see also p. 55*
CHENG, K.C.; YUEN, F.P.*
Flow visualization studies on secondary flow patterns in straight tubes downstream of a 180 deg bend and in isothermally heated horizontal tubes*
J. Heat Transfer 109, 49*
1987. `
..29.6: several types of camera or photodiode array*
WINTER, M.; LAM, J.K.; LONG, M.B.*
Techniques for high-speed digital imaging of gas concentrations in turbulent flows*
Expts. in Fluids 5, 177*
1987. `
..29.6: TiCl4, and mixed with CCl4 as cleaning agent*
BIENKIEWICZ, B.; CERMAK, J.E.*
A flow visualisation technique for low-speed wind-tunnel studies*
Expts. in Fluids 5, 212*
1987. `
..29.6: fibre optics connection to fixed laser*
KOGA, D.J.; ABRAHAMSON, S.D.; EATON, J.K.*
Development of a portable laser sheet*
Expts. in Fluids 5, 215*
1987. `
..29.2: chamfered tube plus pitot - mechanical version*
CHU, J.K.; RIOS-CHIQUETE, E.; SAROHIA, S.; BERNSTEIN, L.*
The "Chu-tube" - a velocimeter for use in highly-sheared, three-dimensional steady flows*
Aero. J. 91, 142*
1987. `
..29.1,30.1,28.3: 4 micro-controlled degrees of freedom*
SHAYESTEH, M.V.; BRADSHAW, P.*
Microcomputer-controlled traverse gear for three-dimensional flow explorations*
J. Phys. E - Sci. Instrum. 20, 321*
1987. `
..29.2: extension of Haan - see also pages 275 and 335*
HOLMES, J.D.; LEWIS, R.E.*
Optimization of dynamic-pressure-measurement systems. 1. Single point measurements*
J. Wind Engg and Indust. Aero. 25, 249*
1987. `
..29.2,23.0: controlled leak*
GERSTOFT, P.; HANSEN, S.O.*
A new tubing system for the measurement of fluctuating pressures*
J. Wind Engg and Indust. Aero. 25, 335*
1987. `
..32.2,29.6: akin to 2-shot bubble wire*
HANSEN, E.C.*
Quantitative visualization of steady and unsteady flows using spark velocimetry*
Rev. Sci. Instrum. 58, 444*
1987. `
..29.6: preheated air enters evaporation trays*
GRANDMAISON, E.W.; NG, S.; BEEKER, H.A.*
A smoke generation system for fluid dynamics research*
J. Phys. E - Sci. Instrum. 20, 605*
1987. `
..59.2;24.4,29.2: pressure taps on sliding ribbon*
WEIBUST, E.; BERTELRUD, A.; RIDDER, S.O.*
Experimental investigation of laminar separation bubbles and comparison with theory*
J. Aircraft, 24, 291*
1987. `
..30.3,29.6,42.3: just so*
GAD-EL-HAK, M.*
The water towing tank as an experimental facility. An overview*
Expts. in Fluids 5, 289*
1987. `
..30.2,29.2: refers to nozzle pressure gradient, not interference*
MAUGHAN, J.R.; INCROPERA, F.P.*
Secondary flow in horizontal channels heated from below*
Expts. in Fluids 5, 344*
1987. `
..29.6: rotate an eccentric cylindrical lens*
SHLIEN, D.J.*
Inexpensive method of generation of a good quality laser light sheet for flow visualization*
Expts. in Fluids 5, 356*
1987. `
..54.0,59.2,29.6: slot I/O to affect pairing - General Scanning Co. vibrating mirror for light sheet*
GAD-EL-HAK, M.; BLACKWELDER, R.F.*
Control of the discrete vortices from a delta wing*
AIAA J. 25, 1042*
1987. `
..29.4: calibration factor nearly unity*
PAN, H.C.; ZHANG, S.Y.*
Measurement of streamwise vorticity using a vane vorticity meter*
Int. J. Heat and Fluid Flow 8, 72*
1987. `
..59.0,28.1,29.6: 2D Galerkin NS sim. at Re=110 - streaklines, streamlines and particle paths*
EATON, B.E.*
Analysis of laminar vortex shedding behind a circular cylinder by computer-aided flow visualization*
J. Fluid Mech. 180, 117*
1987. `
..29.6: image processing of fringe pattern to get continuous density plot*
WATT, D.W.; VEST, C.M.*
Digital interferometry for flow visualization*
Expts. in Fluids 5, 401*
1987. `
..29.6: phase-locked hydrogen bubble pics*
ONGOREN, A.; CHEN, J.; ROCKWELL, D.*
Multiple time-surface characterization of time-dependent three-dimensional flows*
Expts. in Fluids 5, 418*
1987. `
..29.6: four lenses, but easily adjustable*
DIEMUNSCH, G.; PRENEL, J.P.*
A compact light sheet generator for flow visualisations*
Optics and Laser Tech. 19, 141*
1987. `
..53.0,05.0,29.6: smoke wire (invented by Tani)*
SWEARINGEN, J.D.; BLACKWELDER, R.F.*
The growth and breakdown of streamwise vortices in the presence of a wall*
J. Fluid Mech. 182, 255*
1987. `
..22.2,29.1: just so - Euromech 202*
BERG, B. v. d.; BERTELRUD, A.*
Measurement techniques in low-speed turbulent flows*
Expts. in Fluids 6, 61*
1987. `
..24.4,53.0,29.6: laminar flow viz. in cross section*
PEERHOSSAINI, H.; WESFREID, J.E.*
Experiments on Gortler rolls*
Presented at 6th Symposium on Turbulent Shear Flow, Toulouse, paper no. 2-6*
1987. `
..24.4,53.0,29.6: laminar flow viz. in cross section - see also Toulouse*
PEERHOSSAINI, H.; WESFREID, J.E.*
On the inner structure of streamwise Gortler rolls*
Int J. Heat and Fluid Flow (in press)*
1987. `
..29.3,23.0: just so*
MITSCHE, W.; MIROW, P.; SZODRUCH, J.*
Piezo-electric foils as a means of sensing unsteady surface forces on flow-around bodies*
Presented at 6th Symposium on Turbulent Shear Flow, Toulouse, paper no. 6-2*
1987. `
..31.1,29.5: just so*
CASTRO, I.P.; DIANAT, M.*
A pulsed hot wire probe for near wall measurements*
Presented at 6th Symposium on Turbulent Shear Flow, Toulouse, paper no. 6-3*
1987. `
..29.6: digitized movie*
CICCONE, A.D.; KAWALL, J.G.; KEFFER, J.F.*
Digital image analysis of macroscopic particle motions generated by a turbulent wind*
Presented at 6th Symposium on Turbulent Shear Flow, Toulouse, paper no. 6-5*
1987. `
..29.1,28.3: power-switching ICs - good review, naming brands*
HORN, D.*
Motion control in miniature*
Mech Engg vol. 109, no. 11, p. 44*
1987. `
..29.6: mainly separation bubbles*
MUELLER, T.J.*
The visualization of low speed separated and wake flows*
AIAA-87-2422*
1987. `
..32.2,29.2: Keil tube for fluctuations*
JENKINS, R.C.*
Effects of Pitot probe shape on measurement of flow turbulence*
AIAA J. 25, 889*
1987. `
..29.5: from mean vel. profiles - use a complete wall law, e.g. Spalding, rather than just a log law*
SAETRAN, L.R.*
Comparison of five methods for determination of the wall shear stress*
AIAA J. 25, 1524*
1987. `
..29.5,61.0,59.0: comparison of Preston tube, fence, film, McCroskey gauge and PWA (best, fence next)*
DENGEL, P.; FERNHOLZ, H.H.; HESS, M.*
Skin-friction measurements in two- and three-dimensional highly turbulent flows with separation*
Advances in Turbulence (G. Comte-Bellot and J. Mathieu, Eds.), Springer, p. 470*
1987. `
..29.6: update/revision of book*
MERZKIRCH, W.*
Techniques of flow visualization*
AGARDograph 302*
1987. `
..29.6,62.0,11.4,07.0: wet and dry TiO2*
RIVIR, R.B.; ROQUEMORE, W.M.; McCARTHY, J.W.*
Visualization of film cooling flows using laser sheet light*
AIAA-87-1914*
1987. `
..29.6,11.6,32.2: CARS for temperature, wet-and-dry Ti02*
ROQUEMORE, W.M.; CHEN, L-D; GOSS, L.P.; LYNN, W.F.*
The structure of jet diffusion flames*
Presented at U.S.-France joint workshop on turbulent reactive flows, Rouen*
1987. `
..30.1,29.6: intro by Peake et al, then Nosenchuck and Gharib on flow viz.*
ANON.*
Aerodynamics and relation hydrodynamic studies using water facilities*
AGARD Conf. Proc. No. 413*
1987. `
..30.1,29.6: just so*
SMITH, A.M.O.*
Technical evaluation report on the FDP symposium on "Aerodynamic and Related Hydrodynamic Studies using Water Facilities", AGARD CP 413*
AGARD Adv. Rept. 225*
1987. `
..11.6,32.2,29.6: only finds particles with negligible velocity normal to plane*
LEWIS, G.S.; CANTWELL, B.J.; LECUONA, A.*
The use of particle tracking to obtain planar velocity measurements in an unsteady laminar diffusion flame*
Combustion Institute Paper 87-35*
1987. `
..29.6,28.1: including transforms of tomographic images*
HESSELINK, L.*
Digital image processing in flow visualization*
Ann. Rev. Fluid Mech. 20, 421*
1988. `
..44.2,45.0,29.6: useful intro. - 5-hole probe meas. and oil flow*
RICHARDS, P.G.; JOHNSON, C.G.*
Development of secondary flows in the stator of a model turbine*
Expts. in Fluids 6, 2*
1988. `
..28.1,11.6,29.6: digitized video of Bunsen burner*
ZUCHERMAN, L.; KAWALL, J.G.; KEFFER, J.F.*
Digital image analysis of a turbulent flame*
Expts. in Fluids 6, 16*
1988. `
..28.1,29.6: orthogonal views - 11/750 and IIs image proc.*
RACCA, R.G.; DEWEY, J.M.*
A method for automatic particle tracking in a three-dimensional flow field*
Expts. in Fluids 6, 25*
1988. `
..29.2,23.0: published version - total-p tube plus two x-probes for u,v,w*
GIOVANANGELI, J.P.*
A new method for measuring static pressure fluctuations with application to wind-wave interaction*
Expts. in Fluids 6, 156*
1988. `
..24.4,29.6: in flat-plate wake - inc. details of filtering*
LUSSEYRAN, D.; ROCKWELL, D.*
Estimation of velocity eigenfunction and vorticity distributions from the timeline visualization technique*
Expts. in Fluids 6, 228*
1988. `
..29.1: mainly for 3D flows*
LOFDAHL, L.*
Traverse mechanisms for the determination of Reynolds stresses using hot-wire techniques*
Expts. in Fluids 6, 352*
1988. `
..24.1,29.6: nice flow viz. - pH and LIF - but very low Re*
LASHERAS, J.C.; CHOI, H.*
Three-dimensional instability of a plane free shear layer - an experimental study of the formation and evolution of streamwise vortices*
J. Fluid Mech. 189, 53*
1988. `
..24.1,29.6: VAX 11-780 + VICOM image proc.*
AGUI, J.C.; HESSELINK, L.*
Flow visualization and numerical analysis of a coflowing jet - a three-dimensional approach*
J. Fluid Mech. 191, 19*
1988. `
..29.2: four two-tube yawmeters (manifolded to average the angle) and a pitot*
FREESTONE, M.M.*
Vorticity measurement by a pressure probe*
Aero. J. 92, 29*
1988. `
..29.1,30.1: suck-down plenum*
FOSS, J.F.*
Basic elements in a fluid mechanics laboratory experience - an engineering science approach*
J Basic Engg 110, 9*
1988. `
..29.6: 6mm blue centre, 18 mm green ring, red outer field *
OREN, D.C.; DURRETT, R.P.; FERGUSON, C.R.*
Bullseye color schlieren flow visualization*
Expts. in Fluids 6, 357*
1988. `
..29.6,32.2: just so - see also p.373*
ADAMCZYK, A.A.; RIMAI, L.*
Reconstruction of a 3-dimensional flow field from orthogonal views of seed track video images*
Expts. in Fluids 6, 380*
1988. `
..29.6,28.1: "visual correlation" based on angles between consecutive bubble lines*
KERSTENS, P.J.M.; ROCKWELL, D.*
Ensemble-averaging and correlation techniques for flow visualization images*
Expts. in Fluids 6, 409*
1988. `
..29.5: measures slopes directly with optical lever*
BANDYOPADHYAY, P.R.; WEINSTEIN, L.M.*
A simplified oil-film skin-friction meter*
AIAA-88-3601*
1988. `
..05.0,29.6: suggests sweeps trigger the rest - Kline non placet*
BRODKEY, R.S.; OGUNDE, K.; CHAN, L.K.*
Visualisation and simulation of fluid interactions between large scale motions and the streaky structure in a turbulent boundary layer shear flow*
Presented at Zaric Memorial Seminar on Near-Wall Turbulence, Dubrovnik, Yugoslavia, May 1988 (not in Proc.)*
1988. `
..31.1,29.5: hot film - useful results but nothing spectacular*
BEASLEY, D.E.; FIGLIOLA, R.S.*
A generalised analysis of a local heat flux probe*
J. Phys. E. 21, 316*
1988. `
..29.5,31.1: guard film underneath active one (same area)*
POLYAKOV, A.F.; ET AL.*
Shear stress measurements on heat transfer surfaces*
Dantec Inf. no. 6, p. 12*
1988. `
..11.3,53.0,29.5: St increased by 3*
CRANE, R.I.; SABZVARI, J.*
Liquid crystals mapping of laminar convective heat transfer in the presence of Gortler vortices*
Presented at 2nd UK Nat. Heat Transfer Conference, Glasgow*
1988. `
..29.5: poor*
COOK, W.J.; GIDDINGS, T.A.; MURPHY, J.D.*
Response of hot-element wall shear-stress gages in laminar oscillating flows*
AIAA J. 26, 706*
1988. `
..29.6,24.5: amusing art - work done at Kodak US, author now at Ilford CH*
SCHWEIZER, P.M.*
Visualization of coating flows*
J. Fluid Mech. 193, 285*
1988. `
..59.0,29.1: modulates bi-stable flow - relevant to traverse gear, etc.*
SAKAMOTO, H.; HANLU, H.*
Effect of free-stream turbulence on characteristics of fluctuating forces acting on two square prisms in tendem arrangement*
J. Fluids Engg., 110, 140*
1988. `
..29.6,17.1: just so--but nothing specifically unsteady*
GAD-EL-HAK, M.*
Visualization techniques for unsteady flows - an overview*
J. Fluids Engg., 110, 231*
1988. `
..29.6,11.6:Rayleigh and Mie scattered light - 12 1ns exposures while sweeping laser sheet*
YIP, B.F.; SCHMITT, R.L.; LONG, M.B.*
Instantaneous three-dimensional concentration measurements in turbulent jets and flames*
Optics Letters 13, 96 and Sandia 1987 Annual Report*
1988. `
..29.6,11.6:Raman scattering from methane*
NAMAZIAN, M.; SCHEFER, R.W.; KELLY, J.*
Scalar dissipation measurements in the developing region of a jet*
Combustion and Flame,?? and Sandia 1987 Annual Report*
1988. `
..29.6,61.0: conc. measurements from light scattered by aerosol*
VRANOS, A.; LISCINSKY, D.S.*
Planar imaging of jet mixing in crossflow*
AIAA J. 26, 1297*
1988. `
..29.6: density measurements with spatial resolution of 15 microns*
HAVENER, A.G.*
Holographic measurements of transition and turbulent bursting in supersonic axisymmetric boundary layers*
AIAA J. 26, 1467*
1988. `
..32.2,29.6: photochromics in water - Fourier transform to sort out diffraction from strained hologram*
AGUI, J.C.*
Vorticity studies in flows - global three-dimensional analysis and optical point measurements*
PhD thesis, Aero/Astro Dept., Stanford Univ.*
1988. `
..29.6,32.2: grid of laser beams to excite a Kodak chemical in kerosene*
FALCO, R.E.; CHU, C.C.*
A study of turbulence production using a new photochromic visualization technique*
AFOSR-TR-88-0614, AD-A196 887*
1988. `
..54.0,29.6: 5W Ar laser*
GOPINATH, P.R.; SUNDARAM, S.; ET AL.*
Flow visualization of leading edge vortices on a delta wing by laser sheet technique*
IAA N89-11697, 2*
1988. '
..50.0,11.3: turbulence generated by jet grid*
YOUNG, C.D.; HAN, J.C.*
Effect of jet grid turbulence on turbulent boundary layer heat transfer*
ASME HTD 103, 37*
1988. '
..30.1,24.3: 447 pages - WG09 report.  Trips by Russo, 5 papers on Re extrapolation by Haines and/or Elsenaar*
ANON.*
Boundary layer simulation and control in wind tunnels*
AGARD Advisory Report 224*
1988. `
..11.2,29.6:  RGB calibration*
AKINO, N.; KUNUGI, T.; ET AL.*
Liquid-crystal thermometry based on automatic color evaluation and applications to measure turbulent heat transfer*
Transport Phenomena in Turbulent Flows, (M. Hirata and N. Kasagi, eds.), Hemisphere, p. 807*
1988. `
..29.6,11.6:shadowgraph images used to track interface*
SMUCKLAND, R.N.; SWEENEY, D.W.*
Optical flow computation in combustion image sequences*
Appl. Optics 27, 5213*
1988. `
..29.2,59.2,54.0: moderate effect on bursting position*
PAYNE, F.M.; NG, T.T.; NELSON, R.C.*
Seven hole probe measurement of leading edge vortex flows*
Expts. in Fluids 7, 1*
1989. `
..29.2: independent of dimensionless shear down to 0.03 or less, contrary to Hall/Lighthill drift*
TAVOULARIS, S.; SZYMCZAK, M.*
Displacement effect of square-ended pitot tubes in shear flows*
Expts. in Fluids 7, 33*
1989. `
..29.6,31.3: biacetyl for LIF, and smoke*
KENNEDY, I.M.*
Pulsed laser measurements of particle and vapour concentrations in a turbulent jet*
Expts. in Fluids 7, 49*
1989. `
..29.6,54.0: LIF in water with argon-ion laser*
WARD, K.C.; KATZ, J.*
The topology of the flow structures in the lee of an inclined body of revolution - Parts A and B*
Johns Hopkins University papers*
1989. `
..29.6,18.2: reconstruction of 3D density field from several projections*
LIU, T.C.; MERZKIRCH, W.; OBERSTE-LEHN, K.*
Optical tomography applied to speckle photographic measurement of asymmetric flows with variable density*
Expts. in Fluids 7, 157*
1989. `
..02.2,29.6,12.2: including fractal dimension of interface about 2.36*
PRASAD, R.R.; SREENIVASAN, K.R.*
Scalar interfaces in digital images of turbulent flows*
Expts. in Fluids 7, 259*
1989. `
..29.1,17.1: hydraulic blacksmithery*
AHN, S.; CHOI, K.-Y.; SIMPSON, R.L.*
The design and development of a dynamic plunge-pitch-roll model mount*
AIAA-89-0048*
1989. `
..29.6,11.6: phosphorescence*
BATES, S.C.*
A displaced-line velocity diagnostic and its application in a visualization engine*
Expts. in Fluids 7, 335*
1989. `
..29.6: substitute for expensive million-frames/sec cameras*
PAPAMOSCHOU, D.*
A two-spark schlieren system for very-high velocity measurement*
Expts. in Fluids 7, 354*
1989. `
..54.0,29.6: chopped-off tip - Re up to 1 million in water*
KATZ, J.; GALDO, J.B.*
The effect of surface roughness on the rollup process of tip vortices on a rectangular hydrofoil*
To appear in J. Aircraft*
1989. `
..29.6: relevant to surface oil flow - explains streamwise streaks*
LUDWIEG, H.; HORNUNG, H.*
The instability of a liquid film on a wall exposed to an air flow*
J. Fluid Mech. 200, 217*
1989. `
..24.4,29.6: interferometer for density fluctuation*
AZZAZY, M.; MODARRESS, D.; HALL, R.M.*
Optical boundary-layer transition detection in a transonic wind tunnel*
AIAA J. 27, 405*
1989. `
..29.6,32.2: tunable dye laser - rho, T and U*
FLETCHER, D.G.; McDANIEL, J.C.*
Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting supersonic combustor*
AIAA J. 27, 575*
1989. `
..29.5,23.0: pressure and shear stress can be separated fairly well*
NITSCHE, W.; MIROW, P.; SZODRUCH, J.*
Piezo-electric foils as a means of sensing unsteady surface forces*
Expts. in Fluids 7, 111*
1989. `
..29.6: moving mirror to sweep a sheet - delta vortices as example*
PRENEL, J.P.; PROCAR, R.; EL RHASSOULI, A.*
Three-dimensional flow analysis by means of sequential and volumic laser sheet illumination*
Expts. in Fluids 7, 133*
1989. `
..29.6: multiple flash (short-short-long-short) to show speed and direction of particles*
KHALIGHI, B.*
Quantitative fluid velocity measurements by automatic analysis of flow visualization images*
Expts. in Fluids 7, 142*
1989. `
..29.2: in effect, move each hole to reference positions of axial hole*
LIGRANI, P.; SINGER, B.; BAUN, L.*
Spatial resolution and downwash velocity corrections for multiple-hole pressure probes in complex flows*
Expts. in Fluids 7, 424*
1989. `
..02.2,29.6,28.1: image processing of old Head & Bandyo photos*
BANDYOPADHYAY, P.*
The structure of relaminarizing and separating turbulent boundary layers*
NASA Langley paper, part in FED 217, 75 (1995)*
1989. `
..29.5: simpler receiving optics than Monson*
MULLER, U.R.; FEYZI, F.*
Skin-friction measurements by laser-beam interferometry*
AIAA J. 27, 984*
1989. `
..32.2,29.6: LIF from closely spaced images*
PRASAD, R.R.; SREENIVASAN, K.R.*
Three dimensional imaging of turbulent flows*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..32.2,29.6,11.6: Mie scattering from smoke*
BRAY, K.N.C.; CHEW, T.C.; MALY, R.R.*
Quantitative evaluation of length and time scales of turbulent engine combustion from 2D laser sheets*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..29.1: 12 articles - good review including modern techniques*
GAD-EL-HAK, M. (Ed.)*
Advances in Fluid Mechanics Measurements*
Lecture Notes in Engineering, vol. 45, Springer*
1989. `
..29.1,30.: 10 articles - good review *
GAD-EL-HAK, M. (Ed.)*
Frontiers in Experimental Fluid Mechanics*
Lecture Notes in Engineering, vol. 46, Springer*
1989. `
..44.2,29.2: 5-hole probe, 0.6 mm head size, blade turning angle 107 deg.*
YAMAMOTO, A.; MIMURA, F.*
Interaction mechanism between tip leakage flow and the passage vortex in a linear turbine rotor cascade*
Japanese NAL-TR-983T*
1989. `
..29.2: 1 . 22mm outside diameter*
LIGRANI, P.M.; SINGER, B.A.; BAUN, L.R.*
Miniature five-hole pressure probe for measurement of three mean velocity components in low-speed flows*
J. Phys. E., Sci. Instrum. 22, 868*
1989. `
..29.5: xy-plane torque on cylinder*
GUR, Y.; LEEHEY, P.*
A new wall shear stress gauge*
Expts. in Fluids 8, 145*
1989. `
..32.2,29.6: excitation of biacetyl by sinsoidally-modulated light sheet*
LIU, J.-B.; LIU, C.-S.; SHI, J.-R.*
Simultaneous measurement of temperature, density and velocity in gas flows by modulated photoluminescence*
Expts. in Fluids 8, 199*
1989. `
..11.6,29.6: 2D flow viz. and species conc.*
NAMAZIAN, M.; ET AL.*
Nonpremixed bluff-body burner flow and flame imaging study*
Expts. in Fluids 8, 216*
1989. `
..29.6: charge-injection device (CID) cameras*
OZBELGE, H.O.*
On the surface structure and the hydrodynamics of the Benard cells*
Expts. in Fluids 8, 238*
1989. `
..21.2,29.6: LIF - intermittency factor for concentration lower than in forced jet, reaching 0 . 9 on centre line*
PAPANTONIOU, D.; LIST, E.J.*
Large-scale structure in the far field of buoyant jets*
J. Fluid Mech. 209, 151*
1989. `
..29.6,32.2: three TV cameras - data cycle rate only 10 Hz*
NISHINO, K.; KASAGI, N.; HIRATA, M.*
Three-dimensional particle tracking velocimetry based on automated digital image processing*
J. Fluids Engg. 111, 384*
1989. `
..29.2: construction is as easy as 5 and redundancy helps*
ZILLIAC, G.G.*
Calibration of seven-hole pressure probes for use in fluid flows with large angularity*
NASA TM 102200*
1989. `
..62.0,29.6: very low Re*
STAPOUNTZIS, H.*
Flow visualization of a jet in a turbulent cross flow*
Presented at the 5th Int. Sympo. on Flow Visualization, Prague*
1989. `
..32.2,29.6: PIV -  attention to spatial resolution*
REUSS, D.L.; ADRIAN, R.J.; ET AL.*
Instantaneous planar measurements of velocity and large-scale vorticity and strain rate in an engine using particle-image velocimetry*
SAE Tech Paper 890616*
1989. `
..11.2,29.6:  RGB calibration*
AKINO, N.; KUNUGI, T.; ET AL.*
A study on thermo-camera using a liquid-crystal (Method of multiple regression between color and temperature)*
HTD - Vol. 112, Heat Transfer Measurements, Analysis, and Flow visualization, (R.K. Shah, ed.), ASME, p. 115*
1989. `
..29.1: very comprehensive - from workshop techniques to vacuum technology*
MOORE, J.H; DAVIS, C.C.; COPLAN, M.A.*
Building Scientific Apparatus*
Addison-Wesley*
1989. `
..29.6,32.2: introductory review - see AIAA-94-0046*
CHO, Y.-C.*
Digital image velocimetry*
Applied Optics 28, 740*
1989. `
..29.2: see also AIAA J. 25, 567*
KAZIMIERSKI, Z.; HORODKO, L.*
Total pressure averaging by small-diameter tubes in pulsating flows*
AIAA J. 28, 140*
1990. `
..29.6,46.0,02.1: 18 pairs of photos at short intervals*
UTAMI, T.; BLACKWELDER, R.F.*
Flow visualisation with image processing of three-dimensional features of coherent structures in an open-channel flow*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 289*
1990. `
..01.1,05.0,29.6: review - claims agreement between VITA and level, at least on burst interval*
TIEDERMAN, W.G.*
Eulerian detection of turbulent bursts*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 874*
1990. `
..32.2,29.6: good spatial resolution of conc. of fluorescent tracer*
GASKEY, S.; VACUS, P.; DAVID, R.; VILLERMAUX, J.*
A method for the study of turbulent mixing using fluorescence spectroscopy*
Expts. in Fluids 9, 137*
1990. `
..02.2,29.6,42.1: 7 mW laser beam scanned by square plex. block - mentions Oster-Yamamoto two-bucket technique for getting linear stratification. No mention of Sc*
DE SILVA, I.P.D.; MONTENEGRO, L.; FERNANDO, H.J.S.*
Measurement of interfacial distortions at a stratified entrainment interface*
Expts. in Fluids 9, 174*
1990. `
..29.5: still low*
PY, B.*
Improvement in the frequency response of the electrochemical wall shear stress meter*
Expts. in Fluids 8, 281*
1990. `
..29.6: useful review of biacetyl*
HERMANSON, J.C.; WINTER, M.*
Laser-induced fluorescence imaging of supersonic shear flow*
AIAA 90-0501*
1990. `
..29.6: includes survey of photochromic materials - see also thesis*
AGUI GARCIA, J.C.; HESSELINK, L.*
Application of holography to the measurement of velocity gradients in fluid flows sensitized with photochromic dyes*
Phys. Fluids A2, 688*
1990. `
..12.2,29.6: goes logarithmically to 3 at infinite Schmidt number - good discussion of details*
PRASAD, R.R.; SREENIVASAN, K.R.*
The measurement and interpretation of fractal dimensions of the scalar interface in turbulent flows*
Phys. Fluids A2, 792*
1990. `
..29.6,22.1: large if beam lines up with with hairpins*
TRUMAN, C.R.; LEE, M.J.*
Effects of organized turbulence structures on the phase distortion in a coherent optical beam propagating through a turbulent shear flow*
Phys. Fluids A2, 851*
1990. `
..29.6: radon transform*
WATT, D.W.; VEST, C.M.*
Turbulent flow visualization by interferometric integral imaging and computed tomography*
Expts. in Fluids 8, 301*
1990. `
..29.6: coloured chalk and kerosene*
LU, F.K.; SETTLES, G.S.*
Color surface-flow visualization of fin-generated shock wave boundary-layer interactions*
Expts. in Fluids 8, 352*
1990. `
..24.1,29.6: LDV synchronized with flow viz.*
PANIDES, E.; CHEVRAY, R.*
Vortex dynamics in a plane, moderate-Reynolds-number shear layer*
J. Fluid Mech. 214, 411*
1990. `
..29.6,24.1: details of PLIF*
PAUL, P.H.; VAN CRUYNINGEN, I.; HANSON, R.K.; KYCHAKOFF, G.*
High resolution digital flowfield imaging of jets*
Expts. in Fluids 9, 241*
1990. `
..29.6: all the usual traps and some new ones*
GURSUL, I.; LUSSEYRAN, D.; ROCKWELL, D.*
On interpretation of flow visualization of unsteady shear flows*
Expts. in Fluids 9, 257*
1990. `
..29.6,32.2: good review - flow viz. plus gasdynamic properties*
HILLER, B.; HANSON, R.K.*
Properties of the iodine molecule relevant to laser-induced fluorescence experiments in gas flows*
Expts. in Fluids 10, 1*
1990. `
..29.6,32.2,11.6: just so*
VAN CRUYNINGEN, I.; LOZANO, A.; HANSON, R.K.*
Quantitative imaging of concentration by planar laser-induced fluorescence*
Expts. in Fluids 10, 41*
1990. `
..28.1,29.6: 2D correlation of digitized pictures*
BRAND, A.J.; HESSELINK, L.*
Auto-correlation measurements in three-dimensional fluid flow datasets*
Expts, in Fluids 10, 55*
1990. `
..29.6: iso-concentration surfaces of smoke scanned with traversing laser sheet*
YODA, M.; HESSELINK, L.*
A three-dimensional visualization technique applied to flow around a delta wing*
Expts. in Fluids 10, 102*
1990. `
..24.1,29.16: including 5 cm dia circular smoke wire*
KUSEK, S. M.; CORKE, T. C.; REISENTHEL, P.*
Seeding of helical modes in the initial region of an axisymmetric jet*
Expts. in Fluids 10, 116*
1990. `
..11.3,29.6: rhodamine B. LIF and photomultiplier to measure intensity*
ARCOUMANIS, C.; McGUIRK, J.J.; PALMA, J.M.L.M.*
On the use of fluorescent dyes for concentration measurements in water flows*
Expts. in Fluids 10, 177*
1990. `
..28.1,29.6:  PLOT 3D etc.*
WATSON, V.; WALATKA, P.P.; BANCROFT, G.; PLESSEL, T.; MERRITT, F.*
Visualization of fluid dynamics at NASA Ames*
Computing Systems in Engg. 1, 333*
1990. `
..28.1,29.6:  PLOT 3D etc.*
WATSON, V.; WALATKA, P.P.; BANACROFT, G.; PLESSEL, T.; MERRITT, F.*
Visualization of fluid dynamics at NASA Ames*
Computing Systems in Engg. 1, 333*
1990. `
..29.6,32.2: absorption, LIF, Rayleigh, Raman/CARS - general review*
McKENZIE, R.L.*
Progess in laser-spectroscopic techniques for aerodynamic measurements - an overview*
AIAA-91-0059*
1991. `
..29.5: monitor fringes with CCD array*
SETO, J.; HORNUNG, H.G.*
Internally mounted thin-liquid-film skin-friction meter -comparison with floating element method with and without pressure gradient*
AIAA-91-0060*
1991. `
..32.2,29.3,23.0: typically 200Hz*
BATILL, S.M.; NEBRES, J.V.*
Application of digital filtering techniques to unsteady pressure measurements*
AIAA-91-0061*
1991. `
..18.2,29.6: hypersonics*
BUCK, G.M.*
Surface temperature/heat transfer measurement using a quantitative phosphor thermography system*
AIAA-91-0064*
1991. `
..54.0,29.6: inviscid calcs for spanwise gradient, then integral method - experiments include glycol for surface oil flow. Paynter is interested*
ARNAUD, G.L.; RUSSELL, D.A.*
Symmetry-plane model for turbulent flow with vortex generators*
AIAA-91-0723*
1991. `
..29.6,32.2.: PIV etc*
ADRIAN, R.J.*
Particle-imaging techniques for experimental fluid mechanics*
Ann. Rev. Fluid Mech. 23, 261*
1991. `
..29.6:  quantitative LIF with linear photodiode array*
BRUNGART, T.A.; ET AL.*
A fluorescence technique for measurement of slot injected fluid concentration profiles in a turbulent boundary layer*
Expts. in Fluids 11, 9*
1991. `
..29.5:  numerical solution of nonlinear mass-balance equation to get velocity gradient at wall from measured mass-transfer rate*
MAO, Z.; HANRATTY, T.J.*
Application of an inverse mass transfer method to the measurements of turbulent fluctuations in the velocity gradient at the wall*
Expts. in Fluids 11, 65*
1991. `
..29.6:  mix 100-mesh iron powder with the oil*
FUKAMACHI, N.; OHYA, Y.; NAKAMURA, Y.*
An improvement of the smoke-wire method of flow visualization*
Fluid Dynamics Research 7, 23*
1991. `
..24.1,53.0,29.6:  competition of Taylor-Gortler and Kelvin-Helmholtz*
KARASSO, P.S.; MUNGAL, M.G.*
An experimental study of curved mixing layers - flow visualization using volume rendering*
Ames/Stanford Center for Turbulence Research, Annual Research Briefs - 1990, p. 195*
1991. `
..29.2:  pressure coefficient about 3 for Re of 0 . 1, but Stokes law does not apply to previous work at Re of about 10*
CHEBBI, B.; TAVOULARIS, S.*
Pitot-static tube response at very low Reynolds numbers*
Phys. Fluids A3, 481*
1991. `
..32.2,29.6:  just so - video images. Good review.*
WILLERT, C.E.; GHARIB, M.*
Digital particle image velocimetry*
Expts. in Fluids 10, 181*
1991. `
..32.2,29.6:  spatial correlations between two images - avoids identifying individual particles*
UTAMI, T.; BLACKWELDER, R.F.; UENO, T.*
A cross-correlation technique for velocity field extraction from particulate visualization*
Expts. in Fluids 10, 213*
1991. `
..32.1,29.6:  fan of fringes*
NAQWI, A.A.; REYNOLDS, W.C.*
Measurement of turbulent wall velocity gradients using cylindrical waves of laser light*
Expts. in Fluids 10, 257*
1991. `
..29.6:  what is a vortex - Stuart referenced*
GURSUL, I.; ROCKWELL, D.*
Effect of concentration of vortices on streakline patterns*
Expts. in Fluids 10, 294*
1991. `
..29.6:  just so*
VAN CRUYNINGEN, I.; LOZANO, A.; MUNGAL, M.G.; HANSON, R.K.*
Three-dimensional visualization of temporal flow sequences *
AIAA J. 29, 479*
1991. `
..29.6,59.2:  uses powder-coated smoke wire*
NAKAMURA, Y.; FUKAMACHI, N.*
Visualization of the flow past a frisbee*
Fluid Dynamics Res. 7, 31*
1991. `
..62.0,29.6:  intermittency from smoke*
SAVORY, E.; TOY, N.*
Real-time video analysis of twin jets in a crossflow*
J. Fluids Engg. 113, 68*
1991. `
..29.6,11.2:  micro-capsule liquid crystals - HSI space*
DABIRI, D.; GHARIB, M.*
Digital particle image thermometry - The method and implementation*
Expts. in Fluids 11, 77*
1991. `
..29.6:  alcohol*
CLEMENS, N.T.; MUNGAL, M.G.*
A planar Mie scattering technique for visualizing supersonic mixing flows*
Expts. in Fluids 11, 175*
1991. `
..29.2:  odd - says hole Re doesn't matter, and doesn't use inner layer scaling*
DUCRUET, C.*
A method for correcting wall pressure measurements in subsonic compressible flow*
J. Fluids Engineering 113, 256*
1991. `
..09.1,11.3,29.5:  water calibration leads to underestimates suggesting that Reynolds' analogy fails*
HARBISON, W.L.; PETRIE, H.L.*
Evaluation of flush mounted hot-film sensors for skin friction reduction measurements in viscoelastic polymer solutions*
Expts. in Fluids 11, 243*
1991. `
..29.6:  0.1 mm dia pure titanium pellets projected through flow*
MULLER, R.H.G.; HACKESCHMIDT, M.*
A new method for visualization and measurement of turbulent flow patterns*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 4-1*
1991. `
..0.50,29.6:  flow viz. - seeking horseshoe vortices*
UENO, T.; UTAMI, T.*
Two-dimensional pattern recognition processing of near-wall turbulence*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 4-2*
1991. `
..29.6,32.1:  particles with mirrors, order 50 æm diameter*
FRISH, M.B.; FERGUSON, R.D.*
Water-compatible vorticity vector optical probe*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 4-3*
1991. `
..29.5:  geometrically simple fence*
WEISER, N.; NITSCHE, W.; RENKEN, F.*
Wall shear stress determination by means of obstacle-wires*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 4-5*
1991. `
..29.5,17.1:  electrochemical probes in pipe flow*
MAO, Z.; HANRATTY, T.J.*
Measurements of wall shear rate in large amplitude unsteady reversing flows*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 11-1*
1991. `
..29.5,17.1:  hot film gauges*
MAESTRI, R.D.; TARDU, S.; BINDER, G.*
Wall shear-stress measurements in unsteady turbulent flows in diverging channels*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 11-2*
1991. `
..11.6,29.6:  PLIF imaging of OH*
GUTMARK, E.; PARR, P.; HANSON-PARR, D.M.; SCHADOW, K.C.*
Three-dimensional vortical structure of a turbulent flame*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 31-4*
1991. `
..29.2,23.0:  static probe - aspirated with internal hot wire.  Ability to measure static fluctuations not proven*
KIMURA, M.; ONO, K.; SAIMA, A.*
Experimental investigation of the flow structure near the nozzle*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, poster no. III-8*
1991. `
..44.2,29.6:  phase-average velocity plus surface oil-flow viz. (affected by centrifugal force)*
TILLMAN, T.G.; SIMONICH, J.C.*
Hot wire measurements downstream of a propfan*
J. Prop. Power 7, 776*
1991. `
..29.5:  optical-lever measurement of slope - no interferometer*
BANDYOPADHYAY, P.R.; WEINSTEIN, L.M.*
A reflection-type oil-film skin-friction meter*
Expts. in Fluids 11, 281*
1991. `
..29.5:  calculations and experiment - poor behavior in flow reversal*
VAN STEENHOVEN, A.A.; VAN DER BEUCKEN, F.J.H.M.*
Dynamical analysis of electrochemical wall shear rate measurements*
J. Fluid Mech. 231, 599*
1991. `
..09.2,29.6:  axial-view PIV*
YOUNG, J.B.; HANRATTY, T.J.*
Optical studies on the turbulent motion of solid particles in a pipe flow*
J. Fluid Mech. 231, 665*
1991. `
..28.1,29.6:  PIV resolved at 512 x 512 - knowledge-based analysis using info. on geometry and fluid mech.*
WU, Z.Q.; ET AL.*
An image processing system for quantitatively analyzing the 2-D fluid velocity-field image*
Computers and Fluids 20, 359*
1991. `
..11.6,29.6:  Schlieren, and PLIF for OH*
GUTMARK, E.; PARR, T.P.; HANSON-PARR, D.M.; SCHADOW, K.C.*
Simultaneous OH and Schlieren visualization of premixed flames at the lean blow-out limit*
Expts. in Fluids 12, 10*
1991. `
..24.1,28.1,29.6:  strobe images using CCD camera, 1/500 sec. exposure*
CHAO, Y.C.; JENG, M.S.; HAN, J.M.*
Visualization and image processing of an acoustically excited jet flow*
Expts. in Fluids 12, 29*
1991. `
..05.0,29.6:  straight VITA on hydrogen bubble traces - VITA not very satisfactory*
LU, L.J.; SMITH, C.R.*
Use of flow visualization data to examine spatial-temporal velocity and burst-type characteristics in a turbulent boundary layer*
J. Fluid Mech. 232, 303*
1991. `
..11.1,29.6:  k^-1-p where p goes as Re^1/2 for large Re and Sc to ensure convergence of spectrum integral - mixing is not a steady state*
KERSTEIN, A.R.*
Scaling properties of the viscous-convective scalar spectral subrange in turbulent jets*
Phys. Fluids A3, 1832*
1991. `
..29.6,32.2:  "error bars and rules of thumb" - relevant to any randomly-located measurements (including LDV?)*
ALTMAN, D.B.*
Statistics of optimal particle streak photography*
Phys. Fluids A3, 2132*
1991. `
..29.5,45.0: separate fences for 2 components, and oil recipe. Also 74511-2, 1992. JPJ has*
ROTH, K.W.;GUR, Y.; LEEHEY, P.*
Shear stress measurements and flow visualizationon on an axially symmetric body at a large angle of attack*
M.I.T. Acoustics. and Vib. Lab. Rept 73685-1, 74511-1*
1991. `
..29.6,32.2: straight low-density PTV*
KASAGI, N.; NISHINO, K.*
Probing turbulence with three-dimensional particle-tracing velocimetry*
Experimental Thermal and Fluid Science 4, 601*
1991. `
..29.6: see also a Wright Patt. report by Collicott (Purdue), 1992*
WEINSTEIN, L.m.*
An improved large-field focusing schlieren system*
AIAA 91-0567*
1991. `
..29.2: 4-hole cobra probe*
HOOPER, J.D.; MUSGROVE, A.R.*
Multi-hole pressure probes for the determination of the total velocity vector in turbulent single-phase flow*
4th Int. Sympo. Transport Phenomena in Heat and Mass Transfer, (J.A. Reizes, ed.), Pac. Ctr of Thermal-Fluids Engg, p. 1364*
1991. `
..29.2: dished-end pitot tubes -- inviscid calculations*
ROSSOW, V.J.*
Probe shapes for streamwise momentum and cross-stream turbulence intensity*
AIAA J. Aircraft 28, 741*
1991. `
..29.2: including elliptical section static tubes*
ROSSOW, V.J.*
Probe systems for static pressure and cross-stream turbulence intensity*
AIAA J. Aircraft 28, 750*
1991. `
..29.6,32.2,17.1,54.0:  unsteady vortices from underwater vehicles*
HUANG, T.T.; FRY, D.J.; LIU, H.-L.; KATZ, J.; FU, T.C.*
Simultaneous mapping of the unsteady flowfields by particle displacement velocimetry (PDV)*
Presented at 5th Sympo. on Num. and Phys. Aspects of Aerodynamic Flows, Long Beach*
1992. `
..29.6:  1.5 mm "wire" in settling chamber, coated as usual*
MILLER, L.S.; IRANI, E.*
Simple method of supersonic flow visualization using smoke*
AIAA J. 30, 278*
1992. `
..29.5,45.0: separate fences for 2 components - 30 ml ground TiO2, 120-225 ml kerosene, 10-12 droplets oleic acid for 30-40 m/s. Also 73685-1, 1991*
GUR, Y.; LEEHEY, P.*
Surface flow measurements on an axially symmetric body at large angles of attack*
M.I.T. Acoustics. and Vib. Lab. Rept 74511-2*
1992. `
..29.5,18.2: two piezoceramic disks together - wired to back off normal-pressure signal*
KELLY, G.M.; SIMMONS, J.M.; PAULI, A.*
Skin-friction gauge for use in hypervelocity impulse facilities*
AIAA J. 30, 844*
1992. `
..24.1,21.2,29.6: Titan rocket and a 37 cm dia hydrogen flame - renders scalar surface in x, y, t space*
MUNGAL, M.G.; LOZANO, A.; VAN CRYNINGEN, I.*
Large-scale dynamics in high Reynolds number jets and jet flames*
Expts in Fluids 12, 141*
1992. `
..32.2,29.6: fringe tracing - not as easy as it sounds*
NUBEL, R.*
Computer-aided evaluation method for interferograms*
Expts in Fluids 12, 166*
1992. `
..29.6,21.2: hot-air schlieren and dye*
PASCHEREIT, C.O.; OSTER, D.; LONG, T.A.; FIEDLER, H.E.; WYGNANSKI, I.*
Flow visualization of interactions among large coherent structures in an axisymmetric jet*
Expts in Fluids 12, 188*
1992. `
..29.6: use a bent plastic plate as a lens*
SCHEITLE, H.; WAGNER, S.*
A simple lens-like method of determining small light ray deflections*
Expts in Fluids 12, 208*
1992. `
..11.3,29.6: 10-20 micron capsules uniformly suspended*
OZAWA, M.; MULLER, U.; KIMURA, I.; TAKAMORI, T.*
Flow and temperature measurement of natural convection in a Hele-Shaw cell using a thermo-sensitive liquid-crystal tracer*
Expts in Fluids 12, 213*
1992. `
..29.5: fore-and-aft electrodes*
MAO, Z.; HANRATTY, T.J.*
Measurement of wall shear rate in large amplitude unsteady reversing flows*
Expts in Fluids 12, 342*
1992. `
..29.6: zuck it and see - Univ. Essen.*
PETERS, F.; KURALT, T.; SCHNIDERJAN, J.*
Visualization of water flow by sugar schlieren*
Expts in Fluids 12, 351*
1992. `
..32.2,29.6,54.0: bluff bodies, vortex breakdown - pretty pics.*
ROCKWELL, D.; ET AL.*
Instantaneous structure of unsteady separated flows via particle image velocimetry*
Lehigh Univ. Fluid Mech. Lab. Rept PI-1*
1992. `
..30.1,29.1,59.2: general review from Langley - comments that tunnel design methods are out of date*
GLOSS, B.B.*
Future experimental needs to support applied aerodynamics - a transonic perspective*
AIAA 92-0156*
1992. `
..30.1,29.1,59.2: general review*
OLSON, L.E.*
Future experimental needs in low-speed aerodynamics*
AIAA 92-0157*
1992. `
..30.1,29.1,59.2: general review - examples of large scale effects on optimum flap gap, etc.  Detailed complaints about low productivity of NTF*
LYNCH, F.T.*
Experimental necessities for subsonic transport configuration development*
AIAA 92-0158*
1992. `
..29.1,59.2: ex-Grumman, now at VPI - useful review*
MASON, W.H.*
What we need in experimental aerodynamics - one engineering educator's view (invited)*
AIAA 92-0161*
1992. `
..29.6,32.2: deliberate defocusing so image size is proportional to distance*
WILLERT, C.E.; GHARIB, M.*
Three-dimensional particle imaging with a single camera*
Expts. in Fluids 12, 353*
1992. `
..29.6,32,2: analytical differentiation of interpolated velocity*
SINHA, S.K.; KUHLMAN, P.S.*
Investigating the use of stereoscopic particle streak velocimetry for estimating the three-dimensional vorticity field*
Expts. in Fluids 12, 377*
1992. `
..29.5: belt on flexure-supported cylinders - for supersonic tunnels*
VAKILI, A.D.*
A new skin friction balance and selected measurements*
Expts. in Fluids 12, 401*
1992. `
..05.0,29.6,08.0: mainly on errors in hydrogen bubble technique - injection through holes in surface*
BRAND, A.J.*
The turbulent boundary layer - spanwise structure, evolution of low-velocity regions and response to artificial disturbances*
PhD thesis, TU Delft*
1992. `
..29.6,16.2: multiple injection holes - effective y, plus not clear*
TENSI, J.*
Instantaneous visualization of surface flows*
Expts. in Fluids, 13, 33*
1992. `
..52.0,29.6: smoke wire - vortices appear to penetrate into (stable) jet layer*
FUJISAWA, N.*
Visualization of roll-cell structure in turbulent wall jets along a strongly concave surface*
Expts. in Fluids 13, 70*
1992. `
..61.0,29.6: oil line ahead of obstacle can be either separation or reattachment, depending on saddle point*
HUNG, C.-M.; SUNG, C.-H.; CHEN, C.-L.*
Computation of saddle point of attachment*
AIAA J. 30, 1561*
1992. `
..17.1,59.0,29.6: laser-induced photochemical anemometry (photochromic grid)*
CHU, C.C.; LIAO, Y.-Y.*
A quantitative study of the flow around an impulsively started circular cylinder*
Expts. in Fluids 13, 137*
1992. `
..29.5,16.2,24.4: 64 vapor-deposited films*
AGARWAL, N.K.; ET AL.*
Crossflow vortex and transition measurements by use of multielement hot films*
AIAA J. 30, 2212*
1992. `
..09.2,29.5: for 2-phase flow in general, not specifically skin friction*
OZDEMIR, I.B.; WHITELAW, J.H.*
An optical method for the measurement of unsteady film thickness*
Expts. in Fluids 13, 321*
1992. `
..32.2,29.6: microballoons (presumably closely spherical) for seeding - need uniform optical properties to track fading*
DINKELACKER, F.; ET AL.*
Determination of the third velocity component with PTA using an intensity graded light sheet*
Expts. in Fluids 13, 357*
1992. `
..21.2,29.6: LIF images, Re = 5000*
YODA, M.; HESSELINK, L.; MUNGAL, M.G.*
The evolution and nature of large-scale structures in the turbulent jet*
Phys. Fluids A4, 803*
1992. `
..11.3,29.6: many isotherms from single crystal image - resolution 0.2 deg. C*
CAMCI, C.; KIM, K.; HIPPENSTEELE, S.A.*
A new hue capturing technique for the quantitative interpretation of liquid crystal images used in convective heat transfer studies*
J. Turbomachinery 114, 765*
1992. `
..29.5,31.1: hot wire at y, plus = 2*
FLITTIE, K.J.; COVERT, E.E.*
Unsteady turbulent skin-friction measurement in an adverse pressure gradient*
AIAA J. 30, 2647*
1992. `
..29.6,32.2: better signals than biacetyl - nontoxic*
LOZANO, A.; YIP, B.; HANSON, R.K.*
Acetone - a tracer for concentration measurements in gaseous flows by planar laser-induced fluorescence*
Expts. in Fluids 13, 369*
1992. `
..29.6,02.2: dimension depends on ratio of rms turbulence to flame speed*
SHEPHERD, I.G.; CHENG, R.K.; TALBOT, L.*
Experimental criteria for the determination of fractal parameters of premixed turbulent flames*
Expts. in Fluids 13, 386*
1992. `
..21.2,29.6,11.2: LIF - Sc = 2075*
YODA, M.*
The instantaneous concentration field in the self-similar region of a high Schmidt number round jet*
PhD thesis, Dept. of Aero. and Astro., Stanford Univ.*
1992. `
..24.1,11.2,29.6: water, with a fluorescein family dye*
KARASSO, P.S.; MUNGAL, M.G.*
LIF measurements of scalar mixing in turbulent shear layers*
NASA Ames/Stanford Center for Turb. Research, Ann. Res. Briefs, p. 345*
1992. `
..29.5: just so - static tube parallel to y axis*
MACINTOSH, J.C.; ISAACS, L.T.*
RPT - The Roving Preston Tube*
Proceedings, 11th Australasian Fluid Mechanics Conference, p. 1049*
1992. `
..12.1,29.6: floating element. u, v and uv - no w*
GASSER, D.*
Experimental investigation of strongly retarded turbulent boundary layers*
ETH, Zurich Dissertation no. 9944*
1992. `
..29.3: and several other papers*
McLACHLAN, B.G.; ET AL.*
Pressure sensitive paint use in the supersonic high-sweep oblique wing (SHOW) test*
AIAA 92-2686*
1992. `
..29.5: oil exuded round sides of glass insert with simple interferometer below surface*
SETO, J.; HORNUNG, H.*
Two-directional skin friction measurement utilizing a compact internally-mounted thin-liquid-film skin friction meter*
AIAA 93-0180*
1993. `
..29.3: relevant to manometer tube lag?*
BERG, H.R.v.d.; TEN SELDAM, C.A. ; GULIK, P.S.v.d.*
Compressible laminar flow in a capillary*
J. Fluid Mech. 246, 1*
1993. `
..29.2,23.0: luminescence depends on partial pressure of oxygen - S/N poor below M = 0.4 approx*
McLACHLAN, B.G.; ET AL.*
Surface pressure field mapping using luminescent coatings*
Expts. in Fluids 14, 32*
1993. `
..54.0,29.6: LIF dye tracer - breakdown equated to recirculation*
SPOHN, A.; MORY, M.; HOPFINGER, E.J.*
Observations of vortex breakdown in an open cylindrical container with a rotating bottom*
Expts. in Fluids 14, 70*
1993. `
..29.2: just so*
ZILLIAC, G.G.*
Modelling, calibration, and error analysis of seven-hole pressure probes*
Expts. in Fluids 14, 104*
1993. `
..29.6,05.0: resolution 4.6 wall units.  Useful details of technique*
URUSHIHARA, T.; MEINHART, C.D.; ADRIAN, R.J.*
Investigation of the logarithmic layer in pipe flow using particle image velocimetry*
Near-Wall Turbulent Flows (R.M.C. So, C.G. Speziale, B.E. Launder, Eds.) Elsevier, p. 433*
1993. `
..29.6: discussion of smoke image processing*
DELO, C.; SMITS, A.J.*
Visualization of the three-dimensional, time-evolving scalar concentration field in a low Reynolds number turbulent boundary layer*
Near-Wall Turbulent Flows (R.M.C. So, C.G. Speziale, B.E. Launder, Eds.) Elsevier, p. 573*
1993. `
..29.5,06.0: stack of 3 tubes in log layer, eliminating constant and y-zero*
STORM, P.V.; NEWMAN, B.G.*
A pressure instrument to measure skin friction in turbulent boundary layers on smooth and non-smooth walls*
Aero. J., Royal Aero. Soc. 97, 25*
1993. `
..32.2,29.6: fluorescence of atmos. oxygen excited in two stages by two lasers - one to "write" a line, one to "read" after distortion*
MILES, R.B.; ET AL.*
Fundamental turbulence measurements by RELIEF flow tagging*
AIAA J. 31, 447 (was AIAA 92-0007)*
1993. `
..29.3: photoluminescence - 10% accuracy. Most of this issue is on techniques*
MORRIS, M.J.; ET AL.*
Aerodynamic applications of pressure sensitive paint*
AIAA J. 31, 419*
1993. `
..29.2: internal Endevco transducers, 23 mm dia, 50 psi range*
NAUGHTON, J.W.; CATTAFESTA, L.N.; SETTLES, G.S.*
Miniature, fast-response five hole conical probe for supersonic flowfield measurements*
AIAA J. 31, 453*
1993. `
..29.5: "porous ramp" 5mm square in plan view.  Nearly linear*
WANG, Z.Y.*
Experimental study of a wall shear stress sensor based on a porous element*
Expts. in Fluids 14, 153*
1993. `
..05.0,06.0,29.6: grid of 23 pulsed bubble wires to get u, v, w and hence vorticity*
GRASS, A.J.; ET AL.*
Common vortical structure of turbulent flows over smooth and rough boundaries*
AIAA J. 31, 837*
1993. `
..11.2,12.1,29.6: two box-counting techniques*
CAVALIERE, A.; ET AL.*
Fractal analysis of two-dimensional laser light scattering patterns for the study of spatial distribution of scalar qantities in turbulent fields*
Engg Turbulence Modelling and Expts 2, (W. Rodi and F. Martelli, Eds.) Elsevier, p. 382 *
1993. `
..11.3,29.6: narrow-band crystals - small penetration depth assumed*
CAMCI, C.; ET AL.*
Evaluation of a hue capturing based transient liquid crystal method for high-resolution mapping of convective heat transfer on curved surfaces*
J. Heat Transf. 115, 311*
1993. `
..29.2: 4-hole probe, responds to fluctuations up to 1.5kHz*
MUSGROVE, A.R. De L.; HOOPER, J.D.*
Pressure probe measurement of the turbulent shear stress distribution in a swirling jet*
Presented at 3rd World Conf. on Exptl. Heat Transfer, to appear in Exptl. Thermal and Fluid Sci.*
1993. `
..09.4,29.5: floating-element balance. Percentage reduction increases slightly in adverse pressure gradient*
NIEUWSTADT, F.T.M.; ET AL.*
The reduction of skin friction by riblets under the influence of an adverse pressure gradient*
Expts. in Fluids 15, 17*
1993. `
..29.5: floating element, Preston tube, sublayer fence, wall pulsed wire. "satisfactory" agreement*
GASSER, D.; THOMANN, H.; DENGEL, P.*
Comparison of four methods to measure wall shear stress in a turbulent boundary layer with separation*
Expts. in Fluids 15, 27*
1993. `
..29.6,32.2: twin camera PIV*
PRASAD, A.K.; ADRIAN, R.J.*
Stereoscopic particle image velocimetry applied to liquid flows*
Expts. in Fluids 15, 49*
1993. `
..29.2: Re, M and turbulence - Re affects both gross separation, and details of flow near holes even if nulled. Some flow viz.*
DOMINY, R.G.; HODSON, H.P.*
An investigation of factors influencing the calibration of five-hole probes for 3-D flow measurements*
ASME J. Turbomachinery 115, 513*
1993. `
..18.2,29.5: including discussion of Preston tube calibrations*
WILLIAMS, K.E.; GESSNER, F.B.; HARLOFF, G.J.*
Experimental and numerical investigation of supersonic turbulent flow in an annular duct*
AIAA 93-3123*
1993. `
..29.6,32.2: effect of large gradients and out-of-pattern motions*
HUANG, H.T.; FIELDLER, H.E.; WANG, J.J.*
Limitation and improvement of PIV. Part I. Limitation of conventional techniques due to deformation of particle image patterns*
Expts. in Fluids 15, 168*
1993. `
..29.6: Schlieren etc. from 3D*
YATES, L.A.*
Images constructed from computed flowfields*
AIAA J. 31, 1877*
1993. `
..29.6,45.0: unreliable unless streamwise variation is small*
FINLAY, W.H.; GUO, Y.; OLSEN, D.*
Inferring secondary flows from smoke or dye flow visualization. Two case studies*
Phys. Fluids A5, 2689*
1993. `
..29.5: 5-10 sec.*
HUBNER, J.P.; CARROLL, B.F.*
Thin-oil-film interferometric skin-friction measurements in short-duration supersonic flow*
Expts. in Fluids 15, 315*
1993. `
..29.5: collaboration with DANTEC. Vee probe - not much discussion of frequency response*
SUMER, B.M.; ARNSKOV, M.M.; CHRISTIANSEN, N.; JORGENSEN, F.E.*
Two-component hot-film probe for measurements of wall shear stress*
Expts. in Fluids 15, 380*
1993. `
..29.3: water displaced by known weights*
GANZ, J.; THOMANN, H.*
Calibration of pressure transducer for small pressure differences*
Expts. in Fluids 15, 464*
1993. `
..59.0,29.2: linear*
SZEPESSY, S.; BEARMAN, P.W.*
Analysis of a pressure averaging device for measuring aerodynamic forces on a circular cylinder*
Expts. in Fluids 16, 120*
1993. `
..32.2,29.6: 3-camera system in low-speed water flow*
MALIK, N.A.; DRACOS, T.*
Lagrangian PTV in 3D flows*
Advances in Turbulence IV (F.T.M. Nieuwstadt, ed.), Kluwer, Dordrecht (also Appl. Sci. Res. Vol. 51), p. 161*
1993. `
..29.3: fiber optic sensing of reflection from diaphragm*
LIN, H.; HO, C.-H.*
Optical pressure transducer*
Rev. Sci. Instrum. 64 (7), 1999*
1993. `
..29.4: calibration via nasty integral equation - parameterize?*
LANGSTON, L.S.; KASPER, R.G.*
Analysis of an electromagnetic boundary layer probe for low magnetic Reynolds number flows*
J. Fluids Engg. 115, 726*
1993. `
..05.0,29.6: smoke particles ejected near quasi-streamwise vortices*
PIOMELLI, U.; ET AL.*
Reynolds stress and vorticity in turbulent wall flows*
Appl. Sci. Res. 51, 365*
1993. `
..16.2,29.6: Re, theta = 705, no  real 3D conclusions*
GOLDSTEIN, J.E.; SMITS, A.J.*
Flow visualization of the 3-D, time-evolving structure of a turbulent boundary layer*
Phys. Fluids 6, 577*
1994. `
..32.2,29.6: discussion of error sources*
MILES, R.; ET AL.*
Comparison of RELIEF flow tagging and hot-wire velocimetry for fundamental studies of turbulent free jets*
AIAA 94-0496*
1994. `
..29.6,32.2: useful review*
WESTERWEEL, J.*
Efficient detection of spurious vectors in particle image velocimetry data*
Expts. in Fluids 16, 236*
1994. `
..29.6,32.2: PIV and PLIF with same light sheet*
SIMOENS, S.; AYRAULT, M.*
Concentration flux measurements of a scalar quantity in turbulent flows*
Expts. in Fluids 16, 273*
1994. `
..32.1,29.6: atomizer using glycol-water mix. 1.5 micron particles*
DOMNICK, J.; MARTINUZZI, R.*
A cheap and effective alternative for particle seeding fluid in LDA-applications*
Expts. in Fluids 16, 292*
1994. `
..18.1,29.5: Gaudet's data-reduction technique*
FINLEY, P.J.*
The Preston tube in adiabatic compressible flow*
IC Aero Rept. 94-02*
1994. `
..29.6,32.1: 0 . 1mm thick from slit - diffraction effects small*
DECRE, M.; BUCHLIN, J.M.*
An extra-thin light sheet technique used to investigate meniscus shapes by laser induced fluorescence*
Expts. in Fluids 16, 339*
1994. `
..29.3,23.0: electret microphone - Radio Shack 270-085, 6 mm dia. Not clear what's new*
JOHNSTON, R.T.; SULLIVAN, J.P.*
An inexpensive pressure transducer for the measurement of low amplitude unsteady pressure signals*
Expts. in Fluids 16, 342*
1994. `
..29.5: polarization technique - possible relevance to oil film for skin friction?*
LIU, A.-H.; WAYNER, P.C.; PLAWSKY, J.L.*
Image scanning ellipsometry for measuring the transient, film thickness profiles of draining liquids*
Phys. Fluids 6, 1963*
1994. `
..29.6: detailed investigation of commercial He bubble system - produces buoyant bubbles*
KERHO, M.F.; BRAGG, M.B.*
Neutrally buoyant bubbles used as flow tracers in air*
Expts. in Fluids 16, 393*
1994. `
..29.5,05.0: wire height 85 microns - seems to work*
CHEW, Y.T.; KHOO, B.C.; LI, G.L.*
A time-resolved hot-wire shear stress probe for turbulent flow - use of laminar flow calibration*
Expts. in Fluids 17, 75*
1994. `
..29.5: just so. +/- 5 percent accuracy*
REDA, D.C.; MIRATORE, J.J.*
Measurement of surface stress vectors using liquid crystal coatings*
AIAA J. 32, 1577*
1994. `
..32.2,29.6: general progress report*
HUSSAIN, F.: ET AL.*
Recent innovations in holographic particle velocimetry*
Proc. 7th ONR Propulsion Meeting (G. Roy and P. Givi, eds.), p. 233*
1994. `
..24.1,29.6,18.1: rotating mirror at 350 kHz*
MAHADEVAN, R.; LOTH, E.*
High-speed cinematography of compressible mixing layers*
Expts. in Fluids 17, 179*
1994.`
..32.2,29.6: penalty function for path tracking*
GUEZENNEC, Y.G.; ET AL.*
Algorithms for fully automated three-dimensional particle tracking velocimetry*
Expts. in Fluids 17, 209*
1994. `
..44.1,29.6: approximately colour Schlieren*
ZHANG, X.; COX, C.S.*
Measuring the two-dimensional structure of a wavy water surface optically - a surface gradient detector*
Expts. in Fluids 17, 225*
1994. `
..29.5: simply side by side*
ACKERMAN, J.D.; ET AL.*
Preston-static tubes for the measurement of wall shear stress*
J. Fluids Engg. 116, 645*
1994. `
..29.6,32.1: useful review and data tables*
BUDWIG, R.*
Refractive index matching methods for liquid flow investigations*
Expts. in Fluids 17, 350*
1994. `
..54.0,29.6: hi alpha, lo Re delta*
HUBNER, J.P.; KOMERATH, N.M.*
Visualization of quasi-periodic structures in a vortex flow*
AIAA 94-0624*
1994. `
..18.2,29.5: M up to 0.8. Unsworth calibration of Preston tubes*
MOTALLEBI, F.*
Mean flow study of 2-D subsonic turbulent boundary layers*
AIAA J. 32, 2153*
1994. `
..29.5: thermistor above vacuum cavity*
LIU, C.; TAI, Y.-C.; HUANG, J.-B; HO, C.-M.*
Surface micromachined thermal shear stress sensor*
Presented at ASME Winter Annual Meeting*
1994. `
..29.6,32.2: 30 frames/sec. Fourier-space processing*
CHO, Y.-C.; McLACHLAN, B.G.*
Digital image velocimetry applied to determine instantaneous velocity fields of a moving plate wake*
AIAA-94-0046*
1994. `
..23.0,29.3: Soc. of Photo-Opt. Instrum. Engrs. - review of Ames work*
CHO, Y.-C.*
Fiber optic interferometric sensors for aerospace applications*
SPIE Vol. 2270, 56*
1994. `
..29.6: refraction of light from floor grating produces interferometer-like pattern*
PAL, A.K.; BOSE, B.*
Simple method of supersonic flow visualization using watertable*
AIAA J. 33, 181*
1995. `
..29.6,32.2: transonic PIV*
RAFFEL, M.; ET AL.*
Velocity measurement of compressible air flows utilizing a high-speed video camera* 
Expts. in Fluids 18, 204*
1995. `
..29.6,32.2: "caged" dye molecules released by UV laser beam to mark a line*
LEMPERT, W.R.; MARGEE, K.; GEE, K.R.; HAUGLAND, R.P.*
Flow tagging velocimetry in incompressible flow using photo-activated nonintrusive tracking of molecular motion (PHANTOMM)*
Expts. in Fluids 18, 249*
1995. `
..18.2,29.6: several different techniques - shows bulges and temperature fronts*
SMITH, M.W.; SMITS, A.J.*
Visualization of the structure of supersonic turbulent boundary layers*
Expts. in Fluids 18, 288*
1995. `
..29.2: just the low-Re Pitot tube effect*
ISSA, R.I.*
Rise of total pressure in frictional flow*
AIAA J. 33, 772*
1995. `
..29.1,22.2,13.0: in correspondence he said that a theory with an empirical constant is not a theory*
AHARONI, A.*
Agreement between theory and experiment*
Physics Today vol. 48, no. 6, p. 33, June*
1995. `
..44.2,29.6: multiple smoke wires - detailed sketch of vortex pattern. U. Minn. work*
WANG, H.P.; ET AL.*
Flow visualization in a linear turbine cascade of high performance turbine blades*
ASME 95-GT-7, presented at Turbo Expo 95, Houston*
1995. `
..32.2,29.6: optomistic, with corrections*
LOURENCO, L.; KROTHAPALLI, A.*
On the accuracy of velocity and vorticity measurements with PIV*
Expts in Fluids 18, 421*
1995. `
..29.6,02.2: digitized smoke pictures. "Elongation factors" up to 6 in forced mixing layer at very low Re*
CHEN, T.H.; HANCOCK, R.D.*
Two-dimensional shear-layer entrainment and interface-length measurements*
AIAA J. 33, 949*
1995. `
..29.6,32.2: image-pair processing, for discrete or continuous image*
TOKUMARU, P.T.; DIMOTAKIS, P.E.*
Image correlation velocimetry*
Expts. in Fluids 19, 1*
1995. `
..29.6,29.5: white paint with Rembrand 0.83 disperssant*
AOUABED, H.; LEGENTILHOMME, P.; LEGRAND, J.*
Wall visualization of swirling decaying flow using a dot-paint method*
Expts. in Fluids 19, 43*
1995. `
..29.5,18.1: assumes effective height undependent of M*
FINLEY, P.J.; GAUDET, L.*
The Preston tube in adiabatic compressible flow*
Expts. in Fluids 19, 138*
1995. `
..29.2: error typically 5 percent of absolute pressure near 1 atm.*
LEMOINE, F.; LEPORCQ, B.*
An efficient optical pressure measurement in compressible flows - Laser-induced iodine fluorescence*
Expts. in Fluids 19, 150*
1995. `
..29.5,32.1: Naqwi LDA fan. Rms fluctuation 0.4 of mean*
OBI, S.; INOUE, K.; FURUKAWA, T.; MASUDA, S.*
Experimental study on the statistics of wall shear stress in turbulent channel flows*
Presented at 10th Sympo. on Turbulent Shear Flows, Penn. State, paper 5-19*
1995. `
..29.2: individual 5-tube assemblies are brazed and then ground to 45 deg. Chamfer while being rotated in a lathe - ensures symmetry*
WENDT, B.J.; REICHERT, B.A.*
An inexpensive and effective five-hole probe rake*
Expts in Fluids 19, 295*
1995. `
..29.1: mentions 1993 ISO Guide and AIAA Standard S-071-1995. 95% confidence limits recommended*
COLEMAN, H.W.; STEELE, W.G.*
Engineering application of experimental uncertainty analysis*
AIAA J. 33, 1888*
1995. `
..29.6;32.2: just so - also useful review*
BRUNEAU, S.D.; PAULERY, W.R.*
Measuring unsteady velocity profiles and integral parameters using digital image processing of hydrogen bubble timelines*
J. Fluids Engg 117, 331*
1995. `
..29.5,31.1: same calibration for laminar and turbulent flow, if linearized*
GIBBINGS, J.C.; ET AL.*
The proximity hot-wire probe for measuring surface shear in air flows*
Flow Meas. Instrum. 6, 201*
1995. `
..59.0,18.2,29.6: M=0 . 6 - no shocks. Density contours more useful than smoke which integrates the velocity pattern*
ZHONG, S.; SQUIRE, L.C.*
An interferometric study of organized structures in wakes of circular cylinders*
Expts. in Fluids 20, 91*
1995. `
..29.2: pressure taps upstream and downstream of normal disk*
SCHMIDT, U.*
A differential-pressure probe for velocity measurements in swirling air flows*
Expts. in Fluids 20, 134*
1995. `
..28.1,29.1: analysis of DNS data. Both methods smooth the data but circulation method more accurate*
ABRAHAMSON, S.; LONNES, S.*
Uncertainty in calculating vorticity from 2D velocity fields using circulation and least-squares approaches*
Expts. in Fluids 20, 10*
1995. `
..29.5: refinement of Nitsche method*
JEON, W.P.; KANG, S.H.*
Measurement of transitional boundary layer on a flat plate using a computational Preston tube method*
Expts. in Fluids 20, p. 29*
1995. `
..29.6: non-Newtonian dye resists breakup*
HOYT, J.W.; SELLIN, R.H.J.*
A turbulent-flow dye streak technique*
Expts. in Fluids 20, 38*
1995. `
..23.0,29.2: 4-hole cobra probe, 1.5kHz frequency response, 3mm dia*
HOOPER, J.D.; MUSGROVE, A.R.*
Pressure probe measurements of Reynolds stresses and static pressure fluctuations in developed pipe flow*
Twelfth Australasian Fluid Mechanics Conference, Sydney, p. 565*
1995. `
..23.0,54.0,29.2: 4-hole cobra probe*
HOOPER, J.D.; MUSGROVE, A.R.*
Pressure-velocity correlations in swirling pipe flow*
Twelfth Australasian Fluid Mechanics Conference, Sydney, p. 557*
1995. `
..09.2,29.6: air + smoke, and others - anomalous lift force*
HUSAIN, H.S.; HUSSAIN, F.; GOLDSHTIK, M.*
Anomalous separation of homogenous particle-fluid mixtures - further observations*
Phys. Rev. E 52, 4909*
1995. `
..28.1,32.2,29.6: Laser induced photochemical anemometry (LIPA) marked grid*
HILL, R.B.; KLEWICKI, J.C.*
Data reduction methods for flow tagging velocity measurements*
Expts. in Fluids 20, 142*
1996. `
..32.2,29.6: DPIV - same Re as Eggels et al. DNS*
WESTERWEEL, J.; ET AL.*
Measurement of fully-developed turbulent pipe flow with digital particle image velocimetry*
Expts. in Fluids 20, 165*
1996. `
..29.6: stacks of 10 sucessive Mie scattering images*
ISLAND, T.C.; ET AL.*
Instantaneous three-dimensional flow visualization of a supersonic mixing layer*
Expts. in Fluids 20, 249*
1996. `
..29.5: analytic fit, mainly to Rechenberg 1963*
BECHERT, D.W.*
Calibration of Preston tubes*
AIAA J. 34, 205*
1996. `
..29.1: total of 17 papers in this issue - mainly optical. Pages 433-626*
PITZ, R.W.*
Introduction to aerodynamic measurement technology special section*
AIAA J. 34, 433*
1996. `
..32.2,29.6: monochromatic LIF of iodine vapor*
SMITH, M.W.; ET AL.*
Application of absorption filter planar Doppler velocimetry to sonic and supersonic jets*
AIAA J. 34, 434*
1996. `
..29.2: time constants 0.05 to 2.5 sec.*
CARROLL, B.F.; ET AL.*
Step response of pressure-sensitive paints*
AIAA J. 34, 521*
1996. `
..29.5,32.1: better-than-linear approx. from Taylor series.  LDV measurements*
DURST, F.; ET AL.*
Wall shear stress determination from near-wall mean velocity data in turbulent pipe and channel flows*
Expts. in Fluids 20, 417*
1996. `
..29.6,32.2: new technique - refractive index fluctuations. Merzkirch group*
FEMIN, N.; ET AL.*
Visualization of turbulence anisotropy by single exposure speckle photography*
Expts. in Fluids 20, 476*
1996. `
..29.6: smoke from exploding titanium pellets*
MULLER, R.H.G.; ET AL.*
Visualization and measurement of helicopter rotor flow with swept back tip shapes at hover flight using the "flow visualization gun" time line technique*
Expts. in Fluids 21, 161*
1996. `
..29.6: upgrade of Naqwi*
MILLERD, J.E.; ET AL.*
Holographic sensor for measurement of wall velocity gradients*
Expts. in Fluids 21, 469*
1996. `
..09.2,29.6: small density differences can have cumulative effect on nonuniformity*
YARIN, A.L.; ET AL.*
Distribution of particles suspended in convective flow in differentially heated cavity*
Phys. Fluids 8, 1130*
199/6. `
..32.2,29.6: "integral minimization" formulation - good correlation with DNS. Part 2, results, p.1883*
SU. L.K.; DAHM, W.J.A.*
Scalar imaging velocimetry measurements of the velocity gradient tensor field in turbulent flows. I. Assessment of errors*
Phys. Fluids 8, 1869*
1996. `
..32.2,29.6: video frames syrchronized with laser sheets*
USHIJIMA, S.; TAMIKA, N.*
Three-dimensional particle tracking velocimetry with laser-light sheet scannings*
J. Fluids Engg. 118, 352*
1996. `
..23.0,29.3: size down to 7 wall units. Spectra show a (frequency)^-1 region*
LOFDAHL, L.; KALVESTEN, E.; STEMME, G.*
Small silicon pressure transducers for space-time correlation measurements  in a flat plate boundary layer*
J. Fluids Engg. 118, 457*
1996. `
..28.1,29.6: crudely speaking, natural selection*
KIHM, K.D.; ET AL.*
Adoption of a genetic algorithm (GA) for tomographic reconstruction of line-of-sight optical images*
Expts. in Fluids 22, 137*
1996. `
..32.1,29.6: transparent film down to 85 micron thickness - Eindhoven work*
STEENBERGEN, W.*
Reduction of beam refraction in optical pipe flow experiments by use of sheet-fabricated pipe walls*
Expts. in Fluids 22, 165*
1996. `
..29.6: non-Newtonian dye filaments. Keeps filaments coherent, but...*
HOYT, J.W.; SELLIN, R.H.J.*
Visualization of flow around circular cylinders at high Reynolds numbers*
Engg Turb. Modelling and Expt. 3 (W. Rodi and G. Bergeles, eds.), Elsevier, p. 381*
1996. `
..07.0,29.5: cleanup of Musker profile. Recommends kappa = 0.4055 but differences in C and Pi*
GIBBINGS, J.C.*
On the measurement of skin friction from the turbulent velocity profile*
Flow Meas. Instrum. 7, 99*
1996. `
..29.4: 1mm dia paddle-wheel "micro" turbine - made by spark erosion*
IWASAKI, T.; ET AL.*
Study of a sensor for fuel injection quantity*
SAE Tech Paper 970533*
1997. `
..07.0,29.5: (following Barenblatt, with Re-dependent index). Fits better than log law*
DJENIDI, L.; DUBIEF, Y.; ANTONIA, R.A.*
Advantages of using a power law in a low R_theta turbulent boundary layer*
Expts. in Fluids 22, 348*
1997. `
..29.6,32.2: photoactivated dye then LIF. Large-scale fluctuations decay very slowly*
GUIKEY, J.E.; ET AL.*
Mixing mechanisms in turbulent pipe flow*
Phys Fluids 9, 717*
1997. `
..29.5; liquid crystals - see also p. 615*
REDA, D.C.; ET AL.*
New methodology for the measurement of surface shear stress vector distributions*
AIAA J. 35, 608*
1997. `
..29.5: disputes that it is unreliable, nonquantitative, and superseded by DNS*
KLINE, S.J.*
An assessment of the accuracy of flow visualization*
Unpublished paper, Stanford Univ.*
1997. `
..29.6,32.2: LIF, Rayleigh scattering etc.*
MILES, R.B.; LEMPERT, W.R.*
Quantitative flow visualization in unseeded flows*
Ann. Rev. Fluid Mech. 29, 285*
1997. `
..29.6,54.0,59.2:  folded Schlieren using model surface as one (flat) mirror*
DONOHOE, S.R.; BANNINK, W.J.*
Surface reflective visualizations of shock-wave/vortex interactions above a delta wing*
AIAA J. 35, 1568*
1997. `
..05.0,23.0,29.5,28.1:  surface shear stress from u at y^+ = 7.  Progressive filtering to asymptote to zero k*
KRONAUER, R.E.; ET AL.*
How to estimate the low wavenumber turbulence frequency spectrum*
Expts. in Fluids 23, 353*
1997. `
..29.5:  good accuracy for shear stress of order 1 lb/ft^2 (500 ft/sec with c_f = 0.003).  See also AGARD CP-601*
REDA, D.C.; ET AL.*
Measurement of the continuous pressure and surface shear stress vector distributions beneath an inclined, impinging jet using coating and imaging techniques*
AIAA 97-2489*
1997. `
..32.2,29.6:  water-soluble "supramolecules" - active constituent bromonaphthalene - and other phosphorescents*
KOOCHESFAHANI, M.M.; ET AL.*
Molecular tagging diagnostics for the study of kinematics and mixing in liquid-phase flows*
Developments in Laser Techniques and Fluid Mechanics*
(R.J. Adrian et al., Eds.), Springer-Verlag, p. 1.2.1*
1997. `
..32.2,29.6:  grid of laser beams to excite phosphorescence of biacetyl in nitrogen*
STIER, B.; KOOCHESFAHANI, M.*
Molecular tagging velocimetry in gas phase and its application to jet flows*
ASME Paper FEDSM97-3687*
1997. `
..59.2,29.5:  light fringes in oil film*
ZILLIAC, G.*
Skin friction distribution on a wingtip*
AIAA 98-0584*
1998. `
..29.2:  fuzzy logic better than neural network - just an example of a more general technique*
REDINIOTIS, O.K.; CHRYSANTHAKOPOULOS, G.*
Application of neural networks and fuzzy logic to the calibration of the seven-hole probe*
J. Fluids Engg 120, 95*
1998. `
..29.6,24.4:  guanine flakes in water, with image processing to track spiral turbulence*
LITSCHKE, H.; ROESNER, K.G.*
New experimental methods for turbulent spots and turbulent spirals in the Taylor-Couette flow*
Expts. in Fluids 24, 201*
1998. `
..04.0,07.0,29.5: mom. thickness Re 1000-6000. Floating element for skin friction. Small scatter in mean and turb. meas. Increase in log law C seen at low Re. JPJ has journal.*
OSAKA, H.; KAMEDA, T.; MOCHIZUKI, S.*
Re-examination of the Reynolds-number-effect on the mean flow quantities in a smooth wall turbulent boundary layer*
Proc JSME Int. Conf. on Fluid Engg (JSME, Tokyo, pub. 97-203, 1997), p. 1433. Also JSME Internat. J. B41, 56*
1997. `
..32.2,29.6:  multi-grid image processing algorithms*
KUMAR, S.; BANERJEE, S.*
Development and application of a hierarchical system for digital particle image velocimetry to free-surface turbulence*
Phys. Fluids 10, 160*
1998. `
..16.2,29.5:  review of techniques - oil flow, surface not film etc.*
WETZEL, T.G.; SIMPSON, R.L.; CHESNAKAS, C.J.*
Measurement of three-dimensional crossflow separation*
AIAA J. 36, 557*
1998. `
..29.5,29.2: proof of concept in impinging jet*
REDA, D.C.; ET AL.*
Measurement of continuous pressure and shear distribution using coating and imaging techniques*
AIAA J. 36, 895*
1998. `
..29.5,31.1,17.1:  140 sensors, 14 CTA bridges.  Ni films, electron-beam deposition*
LEE, T.; BASU, S.*
Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors*
Expts. in Fluids 25, 108*
1998. `
..54.0,29.6,59.2:  says centrifuging of seed particles out of vortex core can be important*
LEISHMAN, J.G.; BAGAI, A.*
Challenges in understanding the vortex dynamics of helicopter rotor wakes*
AIAA J. 36, 1130*
1998. `
..29.5:  measure fluorescence intensity, not film thickness - easier than interferometry, e.g. in flight*
LIU, T.; SULLIVAN, J.P.*
Luminescent oil-film skin-friction meter*
AIAA J. 36, 1460*
1998. `
..32.2,29.6:  for PIV etc. Random and bias errors*
FOURAS, A.; SORIA, J.*
Accuracy of out-of-plane vorticity measurements derived from in-plane velocity field data*
Expts in Fluids 25, 409*
1998. `
..29.5:  vector measurement.  Check on effect of viewing angle, etc.*
REDA, D.C.; WILDER, M.C.*
Quantitative and qualitative aspects of the shear-sensitive liquid crystal coating method*
Int. Council Aero. Sciences paper ICAS-98-3.3.2*
1998. `
..32.2,29.6:  100-300 nm seed, 1.5 micron resolution "achievable". Paper in prep. for Expts. in Fluids*
SANTIAGO, J.G.; ET AL.*
A micron-resolution particle image velocimetry system for microfluidics*
Presented at 8th International Symposium on Flow Visualization*
1998. `
..54.0,29.4: ultrasound anemometers (square path, with circulation proportional to difference of clockwise and anticlockwise transit times*
JOHARI, H.; MOREIRA, J.*
Direct measurement of delta-wing vortex circulation*
AIAA J. 36, 2195*
1998. `
..29.3:  polyvinylidenefluoride thin film as for Nitsche 1989.  Adequate sensitivity at 8.6 m/s.  Erratic frequency response*
LEE, I.; SUNG, H.J.*
Development of an array of pressure sensors with PVDF film*
Expts. in Fluids 26, 27*
1999. `
..24.1,32.2,29.6:  PLIF using nitric oxide and acetone as the two tracers.  Mixing statistics deduced at well below the image resolution*
KING, G.F.; DUTTON, J.C.; LUCHT, R.P.*
Instantaneous, quantitative measurements of molecular mixing in the axisymmetric jet near field*
Phys. Fluids 11, 403*
1999. `
..29.2:  two perpendicular disks like disk static probes*
GREEN, S.I.; ROGAK, S.N.*
A multiple disk probe for inexpensive and robust velocimetry*
J. Fluids Engg 121, 446*
1999. `
..61.0,29.6,31.1:  25 deg. swept normal plate.  Pulsed-wire wall stress meter, parallel wires at 0.05 mm from surface*
HANCOCK, P.E.*
Measurements of mean and fluctuating wall shear stress beneath spanwise-invariant separation bubbles*
Expts in Fluids 27, 53*
1999. `
..29.3:  approx. capacitor with fluctuating charge.  1000 Pa = 1v at amplifier output.  60 Hz pickup trouble*
SULLIVAN, C.J.; MUELLER, T.J.*
Polyvinylidene fluoride film sensors for measurement of unsteady pressures on aerodynamic surfaces.  Part I - Design, fabrication, calibration and demonstration*
Expts in Fluids 27, 79*
1999. `
..29.1:  80 pages*
SEITZMAN, J.M.; LUCHT, R.P.*
Introduction to aerodynamic measurement technology - special section*
AIAA J. 37, 665*
1999. `
..29.2:  7-hole probes down to 0.09 mm dia. - conventional fabrication*
REDINIOTIS, O.K.; VIJAYAGOPAL*
Miniature multihole pressure probes and their neural-network-based calibration*
AIAA J. 37, 666*
1999. `
..29.2:  Re effects up to 8000 (based on diameter)*
WENGER, C.W.; DEVENPORT, W.J.*
Seven-hole pressure probe calibration method utilizing look-up error tables*
AIAA J. 37, 675*
1999. `
..29.5:  "Thermal tuft" on silicon membrane with air gap below.  Honami group. Similar to Houdeville, Rech. Aero. 1, 67, 1984*
NAGATA, M.; ET AL.*
Innovative surface micro-machined membrane flow sensor*
ASME/JSME paper FEDSM99-7356*
1999. `
..29.5,05.0,21.3:  Kim et al. Re=180 channel. Taylor's hypothesis "holds very well" with free choice of convection velocity. H. Choi group*
JEON, S.; ET AL.*
Space-time characteristics of the wall shear-stress fluctuations in a low-Reynolds-number channel flow*
Phys. Fluids 11, 3084*
1999. `
..29.3:  4 - 5 micron thickness for fast response*
HUBNER, J.P.; ET AL.*
Pressure-sensitive paint measurements in a shock tube*
Expts. in Fluids 28, 21*
2000. `
..29.5:  just so*
BUTTSWORTH, D.R.; ELSTON, S.J.; JONES, T.V.*
Skin friction measurements on reflective surfaces using nematic liquid crystal*
Expts. in Fluids 28, 64*
2000. `
..29.3:  invited review - authors include Mehta*
BELL, J.H.; ET AL.*
Surface pressure measurements using luminescent coatings*
To appear in Annual Review of Fluid Mechanics, Vol. 33, 2001*
2000. `
..29.3: 3 percent rms accuracy in pressure coefft. at 50 m/s. Interesting historical section*
BROWN, O.C.*
Low-speed pressure measurements using a luminescent coating system*
PhD thesis, Aero./Astro. Dept, Stanford Univ.*
2000.
..25.1:  large perturbations of part of partly-optimized solutions - avoids inadmissible solutions.  Theological implications not discussed*
******au
***tit ?? page
J. Comp. Phys. 160, l39*
2000. `
..29.2,44.2:  fast-response pressure (Cobra-type) and temperature probes - detailed review*
SIEVERDING, C.H.; ET AL.*
Measurement techniques for unsteady flows in turbomachines*
Expts in Fluids 28, 285*
2000. `
..09.4,29.5:  riblets on stationary inner cylinder - "need to minimize curvature"*
HALL, T.; JOSEPH, D.*
Rotating cylinder drag balance with application to riblets*
Expts. in Fluids 29, 215*
2000. `
..29.2:  a.k.a. pressure-sensitive parent or PSP.  General review including some Ames results*
BELL, J.H.; ET AL.*
Surface pressure measurements using luminescent coatings*
Annu. Rev. Fluid Mech. 33, 155*
2001. `
..29.6,02.2:  non-mixing dye streamers*
HOYT, J.W.; SELLIN, R.H.J.*
Three-dimensional visualization of large structures in the turbulent boundary layer*
Expts. in Fluids 30, 295*
2001. `
..24.4,29.6:  hydrogen bubble wire*
LEE, C.B.; FU, S.*
On the formation of the chain of ring-like vortices in a transitional boundary layer*
Expts. in Fluids 30, 354*
2001. `
..29.2:  classical error analysis.  Temperature effects are a main source of error*
LIU, T.; GUILLE, M.; SULLIVAN, J.P.*
Accuracy of pressure-sensitive paint*
AIAA J. 39, 103*
2001. `
..29.6: excellent intro/historical chapter, then details*
SETTLES, G.S.*
Schlieren and Shadowgraph Techniques - Visualizing Phenomena in Transparent Media*
Springer*
2001. `
..59.0,29.5:  Re_H from 3500 to 16000 - upstream BL always turbulent.  Mainly skin friction measurements with wall wires*
SPAZZINI, P.G.; ET AL.*
Unsteady behavior of back-facing step flow*
Expts. in Fluids 30, 551*
2001. `
..29.5,31.1:  wire above slot, 100 micron square in side view*
STURZEBECHER, D.; ANDERS, S.; NITSCHE, W.*
The surface hot wire as a means of measuring mean and fluctuating wall shear stress*
Expts. in Fluids 31, 294*
2001. `
..59.2,29.5:  electrodiffusiion for skin friction (correlation of everybody's data for max. - c_f goes as Re^{-0.57} not -0.5).  Max. rms c_f fluctuation roughly same as max. (-mean)*
TIHON, J.; LEGRAND, J.; LEGENTILHOMME, P.*
Near-wall investigation of backward-facing step flows*
Expts. in Fluids 31, 484*
2001. `
..29.5:  just so - nickel on polyimide*
DESGEORGES, O.; LEE, T.; KAFYEKE, F.*
Expts. in Fluids 32, 37*
2002. `
..29.2:  tests in (weak) shock tubes.  Response fitted by that of an m-order linear system*
PANIAGUA, G.; DENOS, R.*
Digital compensation of pressure sensors in the time domain*
Expts. in Fluids 32, 417*
2002. `