..14.0: first k, eps.*
PRANDTL, L.; WIEGHARDT, K.E.G.*
Uber eine neue Formelsystem fuer die ausgebildete Turbulenz*
Nachrichten der Akad. Wiss, Gottingen, Math.-Phys. Klasse, p. 16*
1945 . `
..13.0: classical paper, written before Nov. 1943. `Chou' in journal, modern spelling is `Zhou'*
CHOU, P.Y.*
On velocity correlations and the solutions of the equations of turbulent fluctuations*
Quart. Appl. Math. 3, 38*
1945 . ` 
..05.0: appendix derives log law by dimensional analysis*
SQUIRE, H.B.*
Reconsideration of the theory of free turbulence*
Phil Mag., Ser. 7, vol. 39, No. 288, p. 1*
1948 . `
..13.0: classical papers - in German*
ROTTA, J.C.*
Statistical theory of inhomogeneous turbulence. Parts 1 and 2
Zeit. fuer Phys. 129, 547 and 131, 51*
1951 . `
..30.1: data fit for 60 < Re < 600 (Re based on vel. though pores). K=6.5Re^{-1/3}(1-beta)/beta^2*
WIEGHARDT, K.E.G.*
On the resistance of screens*
Aero. Quart. (Roy. Aero. Soc.) 4, 186*
1953 . `
..28.1: classical paper*
KLINE, S.J.; McCLINTOCK, F.A.*
Describing uncertainties in single-sample experiments*
ASME Mechanical Engineering, Jan., 3-8*

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 .`
..54.0,24.2,12.2:urtext, quelle etc for horseshoes*
THEODORSEN, T.*
The structure of turbulence*
Funfzig Jahre Grenzschichtforschung (H. Gortler and W. Tollmien, Eds), Vieweg, p. 55*
1955 . `
..12.2,50.0,30.1:  classic experiment*
UBEROI, M.S.*
Effect of wind-tunnel contraction on free-stream turbulence*
J. Aero. Sci. 23, 754*
1956 . `
..07.0:damping function*
VAN DRIEST, E.R.*
On turbulent flow near a wall*
J. Aero. Sci. 23, 1007*
1956 . `
..05.0,07.0,12.1: still useful*
CLAUSER, F.H.*
The turbulent boundary layer*
Adv. Appl. Mech.4, 2*
1956 .`
..22.2: still useful*
ANON.*
The direction of research establishments*
H.M. Stationery Office*
1957 . `
..16.1:characteristics for region of influence*
RAETZ, G.S.*
A method of calculating three-dimensional laminar boundary layers of steady compressible flows*
Northrop Aircraft Inc. Rept. NAI-58-73 (BLC-114)*
1957 .`
..54.0: Burgers vortex and extensions*
ROTT, N.*
On the viscous core of a line vortex*
ZAMP 9b, 543*
1958 .`
..12.2,22.2:  gives Re-stress transport equations but is mainly mixing length.  We have progressed*
YEN, K.T.*
An introduction to the theories of turbulence*
Graduate lecture notes, Rensselaer Polytechnic Institute*
1959 . `
..18.1: refined Van Driest transformation with disposable C, C_1 and Pr_t*
ROTTA, J.C.*
Turbulent boundary layers with heat transfer in compressible flow*
AGARD Rept. 281*
1960 .`
..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 .`
..25.6: SGS model*
SMAGORINSKY, J.*
General circulation experiments with the primitive equations. I. The basic experiment*
Monthly Weather Review 91, 99*
1963. `
..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. `
..23.0: basic theory*
CORCOS, G.M.*
The resolution of pressure in turbulence*
J. Acoust. Soc. Am. 35, 192*
1963. `
..24.1: Kelvin-Helmholz frequency .023U/(initial disp. thickness)*
WILLE, R.*
Contributions to the phenomenology of free jets*
Z. fur Flugwiss. 11, 222*
1963. `
..30.1: still quite up to date, alas*
BRADSHAW, P.; PANKHURST, R.C.*
The design of low-speed wind tunnels*
Prog. Aero. Sci. 5, 1*
1964. `
..55.0: equations for non-collateral flow, plus mean flow meas. in up to 12 deg. diffusers after short entry length*
PIERCE, F.J.*
The turbulent flow at the plane of symmetry of a collateral three-dimensional boundary layer*
J. Basic Engg 86, 227*
1964. `
..29.1,30.1: mainly probes and manometers*
ANON.*
Flow measurement facilities and auxiliary equipment*
AVA and MPI fur Stromungsforschung, Gottingen*
1964. `
..18.2: up to 1400 million*
MOORE, D.R.; HARKNESS, J.*
Experimental investigation of the compressible turbulent boundary layer at very high Reynolds numbers*
AIAA Paper 64-592*
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. `
..24.2,24.7:just so*
STUART, J.T.*
The production of intense shear layers by vortex stretching and convection*
Nat. Phys. Lab., Teddington, England, Aero Rept 1147*
1965. `
..21.3: correction is of order of rms intensity*
HESKESTAD, G.*
A generalized Taylor hypothesis with application for high Reynolds number turbulent shear flows*
J. Appl. Mech. 32, Dec., p. 1*
1965. `
..54.0:"Stuart vortices", psi=ln(C cosh y + A cos x), row of z-wise vortices*
STUART, J.T.*
On finite amplitude oscillations in laminar mixing layers*
J. Fluid Mech. 29, 417*
1967. `
..16.1,59.2:part 1 on infinite wings is p. 55 - need 6 in. rad. of curve. to get turb. BL at 35 deg sweep. Gaster p. 165*
CUMPSTY, N.A.; HEAD, M.R.*
The calculation of three-dimensional tubulent boundary layers. Part 2 - attachment-line flow on an infinite swept wing*
Aero. Quart. 18, 150*
1967. `
..16.2,59.2: Lancaster flight tests - Cumpsty p. 150*
GASTER, M.*
On the flow along swept leading edges*
Aero. Quart. 18, 150*
1967. `
..20.0,21.2: calcs. using Gartshore data*
NEWMAN, B.G.*
Turbulent jets and wakes in a pressure gradient*
Fluid Mech. of Internal Flow (G. Sovran, ed.), Elsevier, p. 170*
1967. `
..49.0,30.1: just so - see Johnston 1998 for a prediction method*
SOVRAN, G.; KLOMP, E.D.*
Experimentally determined optimum geometries for rectilinear diffusers with rectangular, conical or angular cross-section*
Fluid Mech. of Internal Flow (G. Sovran, ed.), Elsevier, p. 270*
1967. `
..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. `
..61.0:  hot wire measurements of mean vel. and longitudinal-component turbulence - plain cyl. base*
VANWAGENEN, R.G.*
A study of axially-symmetric subsonic base flow*
PhD Thesis University of Washington*
1968. `
..59.0,12.1: shows phase of lam/turb response to p.g. - figs 5, 6*
ACHENBACH, E.*
Distribution of local pressure and skin friction around a circular cylinder in crossflow up to Re = 5 million*
J. Fluid Mech. 34, 625*
1968. `
..08.0: results and correlation for bilog. law additive constant*
STEVENSON, T.N.*
Inner region of transpired turbulent boundary layers*
AIAA J. 6, 553*
1968. `
..12.2,14.0: REL told PB that Hinze (p. 24) thought of 4-th order eddy viscosity first*
LUXTON, R.E.; MANTON, M.J.; BANNER, M.L.*
On the concept of eddy viscosity*
Mech. and  Chem. Engg Trans, Inst. Engrs of Australia, vol. MC4, no. 1, p.15*
1968. `
..22.1,24.1: Re/initial-condition effects - 2" and 6" jets howled even with turbulent nozzle BL, full-scale engine didn't, ooops*
BRADSHAW, P.; FLINTOFF, J.L.; MIDDLETON, D.*
Unexplained scale effects in ejector shroud "howling".
J. Sound Vib. 7, 183*
1968. `
..61.0:  "high" means up to 60000, but some results with trips.  Pressure distributions only*
MAXWORTHY, T.*
Experiments on the flow around a sphere at high Reynolds numbers*
J. Appl. Mech. 36, 598*
1969. `
..11.1,05.0: mixing length formulas for linear tau and q*
BRADSHAW, P.*
A note on the "Law of the Wall" for temperature*
NPL Aero Note 1080*
1969. `
..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. `
..25.6,14.0,12.1: discussion of DNS possibilities - 50 million hours on KDF9 for a lab.-scale experiment. Harlow-Nakayama model more hopeful*
COSTIN, G.D.L.*
Numerical study of the growth of turbulence in a uniform shear flow*
Sydney Univ. ME Dept TN F-10*
1969. `
..54.0: nice flow viz*
PIZIALI, R.; TRENKA, A.*
An experimental study of blade tip vortices*
Cornell Aero. Lab. CAL AC-2647-S-1*
1970. `
..14.0: one-eq. TKE model with eddy vis. and weighted-integral von-Karman-like lengthscale*
GAWAIN, T.H.; PRITCHETT, J.W.*
A unified heuristic model of turbulence*
J. Comp. Phys. 5, 383*
1970. `
..23.0,06.0: pinhole mics. Still useful*
BLAKE, W.K.*
Turbulent boundary-layer wall-pressure fluctuations on smooth and rough walls*
J. Fluid Mech. 44, 637*
1970. `
..43.0,21.3: Taylor's hypothesis not good for buoyant plumes*
DAVISON, D.S.*
The translation velocity of convective plumes*
Quart. J. Roy. Met. Soc. 100, 572*
1971. `
..23.0,21.3: just so *
WILLS, J.A.B.*
Measurements of the wave-number/phase velocity spectrum of wall pressure beneath a turbulent boundary layer*
J. Fluid Mech. 45, 65*
1971. `
..08.0,57.0: mean flow only - well behaved bilog law below internal layer*
SIMPSON, R.L.*
The effect of a discontinuity in wall blowing on the turbulent incompressible boundary layer*
Int. J. Heat Mass Transfer 14, 2083*
1971. `
..12.2: Logik der Forschung - Corrsin divides into "exploration" and "verification"*
LUXTON, R.E.*
Theoria of experiment in turbulent flows*
$th Australasian Conf. on Hydraulics and Fluid Mech., Melbourne and U. Sydney ME Dept Kolling Lab. rept. 221*
1971. `
..31.1: bi-directional, receiver wires at right angles to pulsed wire. To first approx., resolves vel. in direction normal to both*
BRADBURY, L.J.S.; CASTRO, I.P.*
A pulsed-wire technique for velocity measurements in highly-turbulent flows*
J. Fluid Mech. 49, 657*
1971. `
..24.1,18.2: The "Langley Curve" for dependence of mixing layer spreading rate on M*
BIRCH, S.F.; EGGERS, J.M.*
Free turbulent shear flows*
NASA SP-321, vol. 1, p. 36*
1972. `
..54.0: still useful - explanation in self-induced pressure gradient*
HALL, M.G.*
Vortex breakdown*
Ann. Rev. Fluid Mech. 4, 195*
1972. `
..25.1,18.1: still a useful review*
GOLDSTEIN, S.*
The Navier-Stokes equations and the bulk viscosity of  simple gases*
J. Math. and Phys. Sci., Univ of Madras, 6, 225 (Bhatnagar anniversary issue)*
1972. `
..05.0,19.2: analogy between wall law and Kolmogorov theory - also briefly in Tennekes and Lumley*
MELLOR, G.L.*
The large Reynolds number asymptotic theory of turbulent boundary layers*
Int. J. Engg Sci. 10, 851*
1972. `
..31.1,32.2:heated wire and 2 parallel pickups 0.1 mm downstream, 0.07 mm apart*
BEGUIER, C.; REY, C.; DUMAS, R.; ASTIER, M.*
A new anemometer probe*
Comptes Rendus 277A, 475*
1973. `
..12.2,19.3,19.4:  regards unpredictability as fairly obvious - Kraichnan DIA calcs.*
HERRING, J.R.; RILEY, J.J.*
Growth of uncertainty in decaying isotropic turbulence*
J. Atmos. Sci. 30, 997*
1973. `
..06.0:  density parameter is ratio of surface plan area to frontal area of roughness.  Data scattered*
SIMPSON, R.L.*
A generalized correlation of roughness density effects on the turbulent boundary layer*
AIAA Journal 11, 242*
1973. `
..30.1: upstream-pointing pyramid*
GIBBINGS, J.C.*
The pyramid gauze diffuser*
Ing.-Arch. 42, 225*
1973. `
..09.1: good physical review*
LUMLEY, J.L. *
Drag reduction in turbulent flow by polymer additives*
J. Polymer Sci. D, Macromol. Revs. 7, 263*
1973. `
..44.2,45.0: effectively inviscid review*
HORLOCK, J.H.; LAKSHMINARAYANA, B.*
Secondary flows - theory, experiment and application in turbomachinery aerodynamics*
Ann. Rev. Fluid Mech. 5, 247*
1973. `
..13.0: Daly and Harlow anisotropic dissipation assumption shot down - the "trek to determinacy"*
CORRSIN, S.*
Comment on "Transport equations in turbulence"*
Phys. Fluids 16, 157*
1973. `
..12.2: sudden but arbitrary distortion - RDT calcs.*
SREENIVASAN, K.R.*
Rapid distortion of axisymmetric turbulence*
Curr. Sci. (India) 42, 632*
1973. `
..24.1,18.2: just so*
BROWN, G.L.; ROSHKO, A.*
On density effects and large structure in turbulent mixing layers*
J. Fluid Mech. 64, 775*
1974. `
..24.1: integrate Biot Savart excluding central 2l where l related to core omega*
WIDNALL, S.E.; BLISS, D.B.*
Self induced motion and stability of concentrated vortex filaments*
Arch. Mech. 26, 459*
1974. `
..25.4: J. Harris, 1982, says better than box grid*
BLOTTNER, W.*
Variable grid scheme*
Comp. Methods in Appl. Mech. and Engg 4, 179*
1974. `
..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. `
..54.0,49.0: linearized theory and mean flow meas.*
NISHI, M.; SENOO, Y.*
Investigation of strength and paths of vortices shed from vortex generators in a pipe and application to conical diffusers*
Bull. JSME 17, 326*
1974. `
..54.0,59.2,32.1: discusses vortex wandering. Says uniformly-distributed particles centrifuged out*
ORLOFF, K.L.*
Trailing vortex wind-tunnel diagnostics with a laser velocimeter*
J. Aircraft 11, 477*
1974. `
..28.1: one of the first of the computer-age reviews - points out that inadequate A/D dynamic range underestimates flatness*
VAN ATTA, C.W.*
Sampling techniques in turbulence measurements*
Ann. Rev. Fluid Mech. 6, 75*
1974. `
..19.2: disapproves of lognormal dissipation*
MANDELBROT, B. B.*
Intermittent turbulence in self-similar cascades - divergence of high moments and dimension of the carrier*
J. Fluid Mech. 62, 331*
1974. `
..14.0: Jones-Launder k, eps. model with new (now-standard) constants*
LAUNDER, B.E.; SHARMA, B.I.*
Application of the energy dissipation model of turbulence to the calculation of flow near a spinning disc*
Letters in Heat and Mass Transf. 1, 131*
1974. `
..22.2: 150 pp. Many wise words, esp. on communication/publication. Tanner Philos. Lib. Q175.Z54*
ZIMAN, J.M.*
Public knowledge. An essay concerning the social dimension of science*
Cambridge U.P.*
1974. `
..13.0,06.0,57.0: simplified Lumley & Khajeh-Nouri stress+dissipation model*
RAO, K.S.; WYNGAARD, J.C.; COTE, O.R.*
The structure of two-dimensional internal layer over a sudden change of surface roughness*
J. Atmos. Sci. 31, 738*
1974. `
..11.6: 8/3 ="3 - 1/3"*
MANDELBROT, B.*
On the geometry of homogenous turbulence, with stress on the fractal dimension of the iso-surfaces of scalars*
J. Fluid Mech. 72, 401*
1975. `
..25.6: dodgy transport eqn for SGS K.E.*
SCHUMANN, U.*
Subgrid scale model for finite difference simulations of turbulent flows in plane channels and annuli*
J. Comp. Phys. 18, 376*
1975. `
..42.3: Johns Hopkins oscillating grids*
WOLANSKI, E.J.; BRUSH, L.M.*
Turbulent entrainment across stable density step structures*
Tellus 27, 259*
1975. `
..50.0,11.3,59.0:Re up to 300000 - "ceiling" above 7-10 percent*
LOWERY, G.W.; VACHON, R.I.*
The effect of turbulence on heat transfer from heated cylinders*
Int. J. Heat and Mass Transf. 18, 1229*
1975. `
..09.2,59.0: briefly, they don't*
HERZINGER, G.A.*
Note on the settling of small particles in a recirculating flow*
AIAA J. 13, 837*
1975. `
..25.7: BL approx OK for small bubbles*
MURPHY, J.D.; PRESLEY, L.L.; ROSE, W.C.*
On the calculation of supersonic separating and reattaching flows*
AGARD-CP-168*
1975. `
..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. `
..11.3,21.2: conventional temp. profile wider than vel. profile but instantaneous boundaries the same*
DAVIES, A.E.; KEFFER, J.F.; BAINES, W.D.*
Spread of a heated plane turbulent jet*
Phys. Fluids 18, 770*
1975. `
..14.0: one eqn. for k, and algebraic l - used for wall layer by several later workers*
NORRIS, H.L.; REYNOLDS, W.C.*
Turbulent channel flow with moving wavy boundary*
Stanford Univ Mech Engg Dept Rept FM-10*
1975. `
..05.0,07.0,15.0: first comment that log law fits better than mixing length in adverse p.g.?*
GALBRAITH, R.A.McD.; HEAD, M.R.*
Eddy viscosity and mixing length from measured boundary layer developments*
Aero. Quart. 26, 133*
1975. `
..53.0: delta/R roughly 0.01 - at least 3 percent change in c_f*
MERONEY, R.N.; BRADSHAW, P.*
Turbulent boundary-layer growth over a longitudinally curved surface*
AIAA J. 13, l448*
1975.
..23.0: one-sided T.E. taper (various, some with separation/vortex streeet)*
BLAKE, W.K.*
A statistical description of pressure and velocity fields at the trailing edges of a flat strut*
David Taylor NSRDC Rept 4241*
1975. `
..23.0:  enormous - protrusion much worse than recess*
HANLY, R.D.*
Effects of transducer flushness on fluctuating surface pressure measurements*
AIAA-75-534*
1975. `
..05.0,16.1: mixing-length formula - recommended only for small departures from collinearity. p. 127 is 35 deg. wing expt.*
BERG, B. van den*
A three-dimensional law of the wall for turbulent shear flows*
J. Fluid Mech. 70, 149*
1975. `
..12.1,05.0:  concentrates on coherent structures and bursts*
WILLMARTH, W.W.*
Structure of turbulence in boundary layers*
Adv. Appl. Mech. 15, 159*
1975. `
..30.2: matched power-law curves*
MOREL, T.*
Comprehensive design of axisymmetric wind-tunnel contractions*
J. Fluids Engg 97, 225*
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. `
..06.0: including skewness and flatness. 50$ on-off square wave bars*
WOOD, D.H.; ANTONIA, R.A.*
Measurements in a turbulent boundary layer over a d-type surface roughness*
ASME J. Appl. Mech. 42, 591*
1975. `
..13.0: argues via TKE eqn. that transport is trace of original vel.-p.g. term in <u_iu_j> transport equation*
LUMLEY, J.L.*
Pressure-strain correlation*
Phys. Fluids 18, 750*
1975. `
..13.0: addition of modeled dissipation equation to Bradshaw Ferriss Atwell shear-stress equation - not worth while since only for thin shear layer*
GOTTLIEB, L.; LARNAES, G.*
A dissipation rate equation and its application to turbulent-boundary-layer calculations*
Danish Center for Appl. Math. and Mech., TU Denmark, Rept. 95*
1975. `
..50.0,48.0: 6 sec^-1 - see also Murthy, Squid Internal Flows Workshop, 1976*
AHMAD, Q.A.; LUXTON, R.E.; ANTONIA, R.A.*
Characteristics of a turbulent boundary layer with an external turbulent uniform shear flow*
J. Fluid Mech. 77, 369*
1976. `
..46.0,07.0:  "laminar equivalent" Reynolds number based on hydraulic diameter*
JONES, O.C.*
An improvement in the calculation of turbulent friction in rectangular ducts*
J. Fluids Engg 98, 173*
1976. `
..28.1: refers to other FFT-based methods*
LARSEN, H.*
An algorithm to compute the sequency-ordered Walsh transform*
IEEE Trans on Acoustics, Speech and Signal Proc. ASSP-24, 335*
1976. `
..25.6: Corrsin suggests deriving p. fluc. from computer solution*
CORRSIN, S.; KOLLMANN, W.*
Preliminary report on sheared cellular motion as a qualitative mode of homogeneous turbulent shear flow*
In "Turbulence in Internal Flows" (Project SQUID workshop, S.N.B. Murthy, Ed., Hemisphere)*
1976. `
..54.0,24.2: Karlsruhe work*
WIMMER, M.*
Experiments on a viscous fluid flow between concentric rotating spheres*
J. Fluid Mech. 78, 317*
1976. `
..28.1: Met Office 2D curve fitting program - ApSimon, M.E.*
SYKES, R.I.; HATTON, L.*
Computation of horizontal trajectories based on the surface geostrophic wind*
Atmos. Env. 10, 925*
1976. `
..62.0,55.0: unstable free stag pt if 2 axi jets impinge on each other*
WITZE, P.O.; DWYER, H.A.*
The turbulent radial jet*
J. Fluid Mech 75, 401*
1976. `
..60.0:building-block expts and companion num. sims. - the way to go*
MARVIN, J.G.*
Experiments planned specifically for developing turbulence models in computations of flow fields around aerodynamic shapes*
AGARD-CP-210, paper 14*
1976. `
..24.1,44.2: weak when velocities unequal so that vel. defect disappears*
BOLDMAN, D.R.; BRINICH, P.F.; GOLDSTEIN, M.E.*
Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities*
J. Fluid Mech 75, 721*
1976. `
..32.1: still useful 20 years later*
DURST, F.; MELLING, A.; WHITELAW, J.H.*
Principles and practice of laser-Doppler anemometry*
Academic Press, New York*
1976. `
..02.1: oblique in x-y plane - hot wire rake and wall-stress film probes. Published in Phys. Fluids?*
BROWN, G.L.; THOMAS, A.S.W.*
Large structure in a turbulent boundary layer*
Univ. Adelaide ME Dept TN 16/76*
1976. `
..30.2: vortex panel method plus BFA TBL model. 2D and axi.*
BORGER, G.G.*
The optimization of wind tunnel contractions for the subsonic range*
Ph.D. Thesis, Ruhr Univ., NASA-TT-F-16899*
1976. `
..31.1: the two agree - contradicting Perry and Morrison, JFM 47, 765 (1971)*
BRUUN, H.H.*
A note on static and dynamic calibration of constant-temperature hot-wire probes*
J. Fluid Mech. 76, 145*
1976. `
..18.2: primary report on M=3 cooled wall - see AGARDograph 263*
LADERMAN, A.J.; DEMETRIADES, A.*
Investigation of the structure of a cooled wall turbulent supersonic boundary layer*
Ford Aeronutronic Division Pub. No. U-6370*
1977. `
..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. `
..43.0: intensities depend only on Z/L*
PANOFSKY, H.A.; TENNEKES, H.; LENSCHON, D.H.; WYNGAARD, J.C.*
The characteristics of turbulent velocity components in the surface layer under convective conditions*
Boundary-Layer Met. 11, 355*
1977. `
..25.5: basic ref to Block - ADI method*
BRILEY, W.R.; McDONALD, H.*
Solution of the multidimensional compressible Navier Stokes equations by a generalized implicit method*
J. Comp. Phys. 24, 372*
1977. `
..25.1,05.0: socratic and pragmatic*
NARASIMHA, R.*
A dialogue concerning the use of matched asymptotic expansions in turbulent flows*
Indian Inst. Sci. Rept 77 FM 15*
1977. `
..25.7:similar to Viegas 78-1165 but JL no better than 0 or 1 eq.*
COAKLEY, T.J.; VIEGAS, J.R.; HORSTMAN, C.C.*
Evaluation of turbulence models for three primary types of shock separated boundary layers*
AIAA-77-0692*
1977. `
..27.2:matches NS, BL and invisc.*
SEGINER, A.; ROSE, W.C.*
An approximate calculation of strong interaction on a transonic airfoil*
AIAA-77-0210*
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. `
..59.2,30.2: just so*
WILLIAMS, B.R.*
Design and testing of a 40 percent thickness-to-chord ratio symmetrical fairing*
RAE Tech. Rept. 77168, ARC 37940*
1977. `
..30.3,44.2: free piston tunnel*
SCHULTZ, D.L.; JONES, T.V.; OLDFIELD, M.L.G.*
A new transient cascade facility for the measurement of heat transfer rates*
Oxford Univ. Engg Lab. Rept. 1207/77*
1977. `
..13.0,14.0: first detailed discussion*
SCHUMANN, U.*
Realizability of Reynolds-stress turbulence models*
Phys. Fluids 20, 721*
1977. `
..56.0,59.0: downstream screen - ill-posed backflow. LDV meas.*
SIMPSON, R.L.; STRICKLAND, J.H.; BARR, P.W.*
Features of a separating turbulent boundary layer in the vicinity of separation*
J. Fluid Mech. 79, 553*
1977. `
..19.3: asymptotic behavior of invariants*
LUMLEY, J.L.; NEWMAN, G.R.*
The return to isotropy of homogeneous turbulence*
J. FLuid Mech. 82, 161*
1977. `
..13.0: k, uv, kL model - refs. to earlier papers*
MEINECKE, E.*
Calculation of free turbulent shear flows with a 3-equation turbulence model of J.C. Rotta*
DLR-FB 77-60*
1977. `
..24.5: sperm's eye view - transcript of cheerful lecture*
PURCELL, E.M.*
Life at low Reynolds number*
Amer. J. Phys. 45, 3*
1977. `
..30.2: matched power-law curves as for axi. (1975)*
MOREL, T.*
Design of two-dimensional wind-tunnel contractions*
J. Fluids Engg 99, 371*
1977. `
..18.2: short version of Laderman and Demetriades 1977*
LADERMAN, A.J.*
Effect of wall temperature on a supersonic turbulent boundary layer*
AIAA J. 16, 723*
1978. `
..13.0,12.2: first appearance of II and III*
LUMLEY, J.L.*
Computational modeling of turbulent flows*
Adv. Appl. Mech. 18, 123 (C.H. Yih, Ed.), Academic*
1978. `
..16.2: 60 deg. curved duct - all six stresses with single rotating wire*
DE GRANDE, G.; HIRSCH, C.*
Three-dimensional incompressible turbulent boundary layers*
Free Univ. Brussels, Fluid Mech. Dept, Rept VUB-STR-8*
1978. `
..42.0,07.0: generalized log law with non-d g x fractional density difference as "Keulegan parameter"*
CSANADY, G.T.*
Turbulent interface layers*
J. Geophys. Res. 83, 2329*
1978. `
..62.0: results up to triples*
GUTMARK, E.; WOLFSHTEIN, M.; WYGNANSKI, I.*
The plane turbulent impinging jet*
J. Fluid Mech. 88, 737*
1978. `
..13.0,21.2: vertical strain*
POPE, S.B.*
An explanation of the turbulent round-jet / plane-jet anomaly*
AIAA J. 16, 279*
1978. `
..31.1:static yaw calibn acceptable*
MULHEARN, P.J.; FINNIGAN, J.J.*
A simple device for dynamic testing of X-configuration hot wire probes*
J. Phys. E. 11, 679*
1978. `
..11.6,24.4: turb scale increases on combustion - just higher nu?*
TAKENO, T.; KOTANI, Y.*
Transition and structure of turbulent jet diffusion flames*
Prog. Astro. and Aero. 58, 19 (Ed. L.A. Kennedy), AIAA*
1978. `
..25.7: Wilcox-Rubesin kL better than eddy vis or Glushkoid k*
VIEGAS, J.R.; HORSTMAN, C.C.*
Comparison of multiequation turbulence models for several shock separated boundary-layer interaction flows*
AIAA-78-1165*
1978. `
..59.2: smoothing p. dist over shock for BL calc needs care*
LYNCH, F.T.*
Recent applications of advanced computational methods in the aerodynamic design of transport aircraft configurations*
Aero. J. 82, 503*
1978. `
..59.0: 3D wakes behind 2D bodies*
GERRARD, J.H.*
The wakes of cylindrical bluff bodies at low Reynolds number*
Phil. Trans. Roy. Soc. 288, 351*
1978. `
..13.0: could be an apology for turbulence modeling. Wass took an early computer course at NPL - see Yates 1997*
WASS, D.*
The changing problems of economic management*
Economic Trends no. 293, p. 97, March*
1978. `
..59.2,60.0,17.1: 18 percent circular arc*
SEEGMILLER, H.L.; MARVIN, J.G.; LEVY, L.L.*
Steady and unsteady transonic flow*
AIAA J. 16, 1262*
1978. `
..12.2, 02.1: spectra prop to k^-2 over wide range. Fractals?*
SAYLES, R.S.; THOMAS, T.R.*
Surface topography as a nonstationary random process*
Nature 271, 431*
1978. `
..22.2: includes the (undefined) Munchausen number as a measure of improbability, esp. that of starting Borda free flow*
BINNIE, A.M.*
Some notes on the study of fluid mechanics in Canbridge, England*
Ann. Rev. Fluid Mech.10, 1*
1978. `
..07.0,48.0: Schoenherr-type skin friction formula, etc*
DEAN, R.B.*
Reynolds number dependence of skin friction and other bulk flow variables in two-dimensional rectangular duct flow*
J. Fluids Engng 100, 215*
1978. `
..05.0,12.1: outer layer collapses above Re_theta = 6000 - inner layer "Re-dependent"*
KARLSSON, R.I.*
Similarity of longitudinal turbulence intensity in flat-plate turbulent boundary layers*
Chalmers Tech. Univ., Inst. for Appl. Thermo. and Fluids, Int. Rept. 78/1*
1978. `
..18.2: further writeup of L. and D. 1977
LADERMAN, A.J.; DEMETRIADES, A.*
Turbulent shear stresses in compressible boundary layers*
AIAA J. 17, 736*
1979. `
..05.0,12.1: outer layer self-preserving above Re_theta = 6000 - inner layer "Re-dependent"*
KARLSSON, R.I.*
Similarity of longitudinal turbulence intensity in flat-plate turbulent boundary layers*
Chalmers Univ. of Tech., Goteborg, Applied Thermo- and Fluids Dept, Int. Rept. 78/1*
1978. `
..54.0: about the latest of the "vortex upset" boom*
FRANCIS, M.S.; KENNEDY, D.A.*
Formation of a trailing vortex*
J. Aircraft 16, 148*
1979. `
..54.0: somewhat theological*
LUGT, H.J.*
The dilemma of defining a vortex*
Theoretical and Experimental Fluid Mechanics, p.309, Springer*
1979. `
..43.1,06.0:just so*
FINNIGAN, J.J.*
Turbulence in waving wheat I and II*
Boundary-Layer Met. 16, 181 and 213*
1979. `
..25.5: upwind methods corrected to give central diff. accuracy*
RICHARDS, C.W.; CRANE, C.M.*
The accuracy of finite difference schemes for the numerical solution of the Navier Stokes equation*
Applied Math. Modelling 3, 205*
1979. `
..22.2,13.0: turbulence is and will remain the most difficult problem of fluid mechanics*
LIEPMANN, H.W.*
The rise and fall of ideas in turbulence*
Amer. Scientist 67, 221, March - April*
1979. `
..22.2:not bad at all - about a quarter of the papers presented*
BRADBURY, L.J.S.; DURST, F.; LAUNDER, B.E.; SCHMIDT, F.W.; WHITELAW, J.H. (Eds.)*
Turbulent Shear Flows 1*
Springer, Berlin*
1979. `
..59.2: including RAE 2822 writeup*
ANON.*
Report on the FDP Working Group 04 on experimental data base for computer program assessment*
AGARD-AR-138*
1979. `
..62.0,14.0: k, eps. for free jets from rect. orifices - refs.*
McGUIRK, J.J.; RODI, W.*
The calculation of three dimensional turbulent free jets*
Turbulent Shear Flows 1 (Ed. F. Durst et al., Springer), p. 71*
1979. `
..45.1: 180 deg, but AR=13*
LESCHZINER, M.A.; RODI, W.*
Calculation of strongly curved open channel flow*
Proc. ASCE 105, HY10, 1297*
1979. `
..31.1:mean vel profile OK, unlike Antonia Expts in Fluids, 3, 121*
SUBRAMANIAN, C.S.; ANTONIA, R.A.*
Statistical properties of temperature in the wall region of a turbulent boundary layer*
Trans. CSME 5, 221*
1979. `
..25.5:stress relaxation equation*
HOKENSEN, G.*
Transport physics and mathematical characteristics*
AIAA J. 17, 781*
1979. `
..02.2:still Gaussian - interface flatter than in far wake*
KAWALL, J.G.; KEFFER, J.F.*
Interface statistics of a uniformly distorted heated turbulent wake*
Phys. Fluids 22, 31*
1979. `
..48.0:cf(z) modulated by unsteadiness, I reckon - slow wanderings*
NAGANO, Y.; HISHIDA, M.; KAJI, N.*
Structure of mean velocity fluctuation and its influence on turbulence characteristics in the entrance region of a pipe*
Bull. Jap. Soc. Mech. Engrs 22, 1754*
1979. `
..60.0: flow viz. and p. dists*
KUBOTA, H.*
A flow field model of the glancing shock and turbulent boundary layer interaction region*
Cranfield C. of A. Memo. 7901, AFOSR-76-3006 B*
1979. `
..60.0:incident shock at or near expansion corner*
CHEW, Y.T.; SQUIRE, L.C.*
The boundary layer development downstream of a shock interaction at an expansion corner*
ARC R. and M. 3839*
1979. `
..27.4:matches at y=delta near TE, but only to avoid invisc. odds*
OSKAM, B.*
A calculation method for the viscous flow around multi-component airfoils*
NLR TR 79097U*
1979. `
..31.1:*
SIMPSON, R.L.; HEIZER, K.W.; NASBURG, R.E.*
Performance characteristics of a simple linearized hot-wire anemometer.*
J. Fluids Engg 101, 381*
1979. `
..31.1:*
BRISON, J.F.; CHARNAY, J.; COMTE-BELLOT, G.*
Calcul des transports thermiques entre film chaud et substrat par un modele a deux dimensions.*
Int. J. Heat Mass Transf. 22, 111*
1979. `
..31.2:*
ROOS, F.W.*
Hot-film probe technique for monitoring shock-wave oscillations.*
J. Aircraft 16, 871*
1979. `
..27.1: hamfisted Interactive Zone Imbedding*
LEVY, R.; BRILEY, W.R.; McDONALD, H.*
Viscous flow in the region of a rounded trailing edge.*
Sci. Res. Assoc. Rept. R79-920003-F.*
1979. `
..43.0:book*
McBEAN, G.A. (Ed.)*
The planetary boundary layer.*
World Met. Org. TN165*
1979. `
..62.0: see 28, 1397 (1985)*
SUGIYAMA, Y.; USAMI, Y.*
Expts. on the flow in and around jets directed normal to a cross flow*
Bull. JSME 22, 1737*
1979. `
..16.1:non-invariant "T" model*
ROTTA, J.C.*
A family of turbulence models for three-dimensional boundary layers*
Turbulent Shear Flows I (F. Durst et al., eds.) Springer, p. 267*
1979. `
..30.3:3m x 2m,contraction ratio about 2 to 1 - see Watkins 1984*
HIRD, T.G.*
The design and construction of an industrial wind tunnel*
Royal Melbourne Inst. of Tech. Rept 114001R*
1979. `
..19.2,21.2: blames large-scale structures for anomalous T derivatives - small scales are isotropic*
SREENIVASAN, K.R.; ANTONIA, R.A.; BRITZ, D.*
Local isotropy and large structuress in a heated turbulent jet*
J. Fluid Mech. 94, 745*
1979. `
..07.0: 1/Ky+.001093y^3 fits 1/nu_t - approved by Coles*
MUSKER, A.J.*
Complete expression for the smooth wall velocity distribution in a turbulent boundary layer*
AIAA J. 17, 655*
1979. `
..18.1,07.0: claims Pi decreases at high Re - not much later confirmation*
MABEY, D.G.*
Influence of the wake component on turbulent skin friction at subsonic and supersonic speeds*
Aero. Quart. 30, 590*
1979. `
..32.1: still useful for basic theory 15 years later*
BUCHHAVE, P.; GEORGE, W.K.; LUMLEY, J.L.*
The measurement of turbulnce with the laser-Doppler anemometer*
Ann. Rev. Fluid Mech. 11, 443*
1979. `
..43.1,11.2:  not due to buoyancy*
ANTONIA, R.A.; CHAMBERS, A.J.*
Temperature ramps in the atmospheric surface layer*
J. Atmos. Sci. 36, 99*
1979. `
..42.3: 1/3 power law for U, -1/3 for T, in "inner layer"*
GEORGE, W.K.; CAPP, S.P.*
A theory for natural convection boundary layers next to heated vertical surfaces*
Int. J. Heat Mass Transf. 22, 813*
1979. `
..30.2: including charts for wide-angle diffusers*
MEHTA, R.D.; BRADSHAW, P.*
Design rules for small low speed wind tunnels*
Aero. J. (Royal Aeronautical Soc.) 73, 443*
1979. `
..01.1: effect of prob. dist. truncated by threshold*
HAVERBEKE, A.; WOOD, D.H.; SMITS, A.J.*
Uncertainties and errors in conditional sampling*
Presented at 2nd Int. Sympo. on Turb. Shear Flows, London, paper 1.11*
1979. `
..12.1: mean vel., and xy-plane stresses and triples, tabulated. BL thickness as large as 1/4 test-section width*
EAST, L.F.; SAWYER, W.G.; NASH, C.R.*
An investigation of the structure of equilibrium turbulent boundary layers*
Royal Aircraft Estab. (DERA) TR 79040*
1979. `
..12.2,25.1: general review (Warwick U.)*
ZEEMAN, E.C.*
Bifurcation, catastrophe and turbulence*
Conf. on New Directions in Applied Mathematics, Case W.R. Univ., Springer Lecture Notes in Math.*
1980. `
..06.0:  mod. roughness Re including skewness, kurtosis.  Difference between ship roughness and Nikuradse's uniform sand*
MUSKER, A.J.*
Universal roughness functions for naturally-occurring surfaces*
Transactions Canadian Soc. of Mech. Eng. 6, 1*
1980. `
..19.2: zither, a.k.a. mandoline*
KELLOGG, R.M.; CORRSIN, S.*
Evolution of a spectrally local disturbance in grid-generated, nearly isotropic turbulence*
J. Fluid Mech. 96, 641*
1980. `
..12.2: RDT*
TOWNSEND, A.A.*
The response of sheared turbulence to additional distortion*
J. Fluid Mech. 98, 171*
1980. `
..30.2,50.0: at large scale, "blocking effect" may even lead to decrease in intensity*
GOLDSTEIN, M.E.; DURBIN, P.A.*
The effect of finite turbulence spatial scale on the amplification of turbulence by a contracting stream*
J. Fluid Mech. 98, 473*
1980. `
..04.0: scruffy*
BARR, P.K.*
Calculation of skin-friction coefficients for low-Reynolds-number turbulent boundary layer flow.*
Sandia Labs Rept SAND-79-8062*
1980. `
..50.0: quadratic*
MEIER, H.U.; KREPLIN, H.P.*
Influence of freestream turbulence on boundary layer development*
AIAA J. 18, 11*
1980. `
..59.2:*
SPAID, F.W.; STIVERS, L.S.*
Supercritical aerofoil boundary layer measurements.*
J. Aircraft 17, 567*
1980. `
..12.1,30.2:useful calcs and expts*
TULAPURKARA, E.G.; RAMJEE, V.*
Effect of contraction on screen-generated turbulence.*
Aero. J. 84, 290*
1980. `
..54.0:different vortex modes*
SILBERMAN, E.*
Turbulence in helically corrugated pipe flow.*
Proc.ASCE 106, EM4, 699*
1980. `
..50.0:final rept, inc heat transfer*
BLAIR, M.F.; WERLE, M.J.*
The influence of free-stream turbulence on zero pressure gradient fully turbulent boundary layer.*
United Tech. Res. Center R80-914388-12*
1980. `
..19.1,42.3: Re, lambda of 60 from towed grid in vertical water tank*
DICKEY, T.D.; MELLOR, G.L.*
Decaying turbulence in neutral and stratified fluids*
J. Fluid Mech. 99, 13*
1980. `
..24.4,01.2:contours of T perturbations*
VAN ATTA, C.W.; HELLAND, K.N.*
Exploratory temperature-tagging measurements of turbulent spots in a heated laminar boundary layer.*
J. Fluid Mech. 100, 243*
1980. `
..11.3: inhomo. grid expt, with uv really near zero*
GILBERT, B.*
Diffusion mixing in grid turbulence without mean shear.*
J. Fluid Mech. 100, 349*
1980. `
..24.1:*
HUSSAIN, A.K.M.F.; THOMPSON, C.A.*
Controlled symmetric perturbation of the plane jet -an experimental study in the initial region.*
J. Fluid Mech. 100, 397*
1980. `
..44.2: Penn State*
RAVINDRANATH, A.; LAKSHMINARAYANA, B.*
Mean velocity and decay characteristics of the near and far wake of a compressor rotor blade at moderate loading.*
J. Engg Power 102, 535*
1980. `
..59.2: Boeing*
TJONNELAND, E.; BIRCH, S.F.*
Application of viscous analysis to the design of jet exhaust powered lift installations.*
J. Engg Power 102, 626*
1980. `
..29.6:ARL*
POLLOCK, N.*
A simple laser interferometer for wind tunnel flow visualization.*
J. Phys. E, 13, 1062*
1980. `
..31.1: a few cm per sec*
MAHAJAN, R.L.; GEBHART, B.*
Hot-wire anemometer calibration in pressurized nitrogen at low velocities.*
J. Phys. E, 13, 1110*
1980. `
..30.2: including large wake region*
GILBERT, B.*
Turbulent flows produced by perforated plate generators in wind tunnels*
AIAA J. 18, 275*
1980. `
..48.0,27.1: inner and outer expansion - says JA ignorant on log law*
ALBER, I.E.*
Turbulent wake of a thin, flat plate.*
AIAA J. 18, 1044*
1980. `
..21.2: u, T and prob dists*
ANTONIA, R.A.; RAJAGOPALAN, S.*
Characteristics of a mixing layer of a two-dimensional turbulent jet.*
AIAA J. 18, 1052*
1980. `
..59.0,06.0: roughness - Re up to 10 million*
JAMES, W.D.; PARIS, S.W.; MALCOLM, G.N.*
Study of viscous crossflow effects on circular cylinders at high Reynolds numbers.*
AIAA J. 18, 1066*
1980. `
..24.1: nothing new*
ROSHKO, A.*
The plane mixing layer. Flow visualization results and three-dimensional effects.*
Paper presented at International Conf. on Coherent Structures, UAN-IBM Scientific Center, Madrid*
1980. `
..42.3:circ-cyl-like bifurcation*
GOLLUB, J. P.; BENSON, S.V.*
Many routes to turbulent convection.*
J. Fluid Mech. 100, 449*
1980. `
..24.4:low freq - pathological, being transn*
RAMAPRIAN, B.R.; TU, S-W.*
An experimental study of oscillatory pipe flow at transitional Reynolds numbers.*
J. Fluid Mech. 100, 513*
1980. `
..19.1,11.3: mandoline like*
SREENIVASAN, K.R.; TAVOULARIS, S.; HENRY, R.; CORRSIN,S.*
Temperature fluctuations and scales in grid-generated turbulence.*
J. Fluid Mech. 100, 597*
1980. `
..48.0:*
ANDREOPOULOS, J.; BRADSHAW, P.*
Measurements of interacting turbulent shear layers in the near wake of a flat plate.*
J. Fluid Mech. 100, 639*
1980. `
..21.2: Lorenz-Mie scattering - see also AIAA-80-1370*
LONG, M.B.; CHU, B.T.*
On the mixing and structure of an axisymmetric turbulent mixing layer.*
AIAA-80-1354*
1980. `
..45.0,27.3:*
BRILEY, W.R.; McDONALD, H.*
Computation of three-dimensional horseshoe vortex flow using the Navier-Stokes equations.*
7th Int.Conf. on Numerical Methods in Fluid Dynamics, NASA-Ames Research Centre*
1980. `
..47.2,16.1:*
MARKATOS, N.C.; MALIN, M.R.; TATCHELL, D.G.*
Computer analysis of three-dimensional turbulent flows around ships' hulls.*
Proc. I. Mech. E. 194, 239*
1980. `
..24.1: more pretty pics*
SCHNEIDER, P.E.M.*
Secondary vortices in ring vortices and in jets*
Z. Flugwiss. 4, 307*
1980. `
..19.2: mu = 0.25 for Re, lambda greater than 200*
VAN ATTA, C.W.; ANTONIA, R.A.*
Reynolds number dependence of skewness and flatness factors of turbulent velocity derivatives*
Phys. Fluids 23, 252*
1980. `
..13.0: frame invariance*
SPEZIALE, C.G.*
Closure relations for the pressure strain correlation of turbulence*
Phys. Fluids 23, 459*
1980. `
..24.1:*
MILES, J.W.*
On Kelvin-Helmholtz instability.*
Phys. Fluids 23, 1915*
1980. `
..19.1,42.3: grid dropped through interface*
LINDEN, P.F.*
Mixing across a density interface produced by grid turbulence.*
J. Fluid Mech. 100, 691*
1980. `
..24.1: 2D num sim - no pairing*
AREF, H.; SIGGIA, E.D.*
Vortex dynamics of the two-dimensional turbulent shear layer.*
J. Fluid Mech. 100, 705*
1980. `
..57.0:*
ASWATHA NARAYANA, P.A.*
An investigation of a turbulent boundary layer on a flat plate with a small step change in surface roughness.*
Aero. Quart. 31, 221*
1980. `
..46.0:*
MARSTERS, G.F.; FOTHERINGHAM, J.*
The influence of aspect ratio on incompressible turbulent flows from rectangular slots.*
Aero. Quart. 31, 285*
1980. `
..25.10:general chat*
BRANDT, A.*
Multilevel adaptive computations in fluid dynamics.*
AIAA J. 18, 1165*
1980. `
..18.2: The two curved ramps - AIAA-79-1563*
LADERMAN, A.J.*
Adverse pressure gradient effects on supersonic boundary-layer turbulence.*
AIAA J. 18, 1186*
1980. `
..25.10: spacing inverse to dU/dy say*
DWYER, H.A.; KEE, R.J.; SANDERS, B.R.*
Adaptive grid method for problems in fluid mechanics and heat transfer.*
AIAA J. 18, 1205*
1980. `
..11.6: Book - see also AIAA J. 19 261 (1981)*
LIBBY, P.A.; WILLIAMS, F.A.*
Turbulent reacting flows.*
Topics in Applied Physics 44, Springer, Berlin*
1980. `
..30.2: not very clever*
JACOBS, P.P.*
A method of correcting for the effects of the side wall boundary layer in two-dimensional aerofoil testing.*
Penn. State Univ. ARL/PSU/TM/80/44, AD/A086079*
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. `
..08.0:Reynolds stress meas*
YAVUZKURT, S.; MOFFAT, R.J.; KAYS, W.M.*
Full-coverage film cooling.*
J. Fluid Mech. 101, 129*
1980. `
..46.0,51.0,61.0,62.0: parallel to surface - becomes 3D wall jet*
DAVIS, M.R.; WINARTO, H.*
Jet diffusion from a circular nozzle above a solid plane.*
J. Fluid Mech. 101, 201*
1980. `
..47.2:*
ODABASI, A.Y.; SAYLAN, O.*
GEMAK - a method for calculating the flow around aft-end of ships.*
13th Symp. on Naval Hydrodynamics, Tokyo, Paper 7-4*
1980. `
..24.1:*
BREIDENTHAL, R.*
Response of plane shear layers and wakes to strong three-dimensional disturbances.*
Phys. Fluids 23, 1929*
1980. `
..26.2:*
CAUGHEY, D.A.; JAMESON, A.*
Progress in finite-volume calculations for wing-fuselage combinations.*
AIAA J. 18, 1281*
1980. `
..18.1,15.0:variable K and everything else*
JOBE, C.E.; HANKEY, W.L.*
Turbulent boundary-layer calculations in adverse pressure gradient flows.*
AIAA J. 18, 1394*
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. `
..54.1: synoptic - 0,1 and 2-eqn models*
RAJ, P.; IVERSEN, J. D.*
Computational simulation of turbulent vortex merger and decay.*
AIAA J. 18, 865*
1980. `
..25.4,27.1: inverse soln. in iteration loop*
ARIELI, R.; MURPHY, J. D.*
Pseudodirect solution to the boundary layer equations for separated flow.*
AIAA J. 18, 883*
1980. `
..48.0,21.3: Urbana - X-film Marseillaise*
HASSAN, Y.A.; JONES, B.G.; ADRIAN, R.J.*
Measurements and axisymmetric model of spatial correlations in turbulent pipe flow.*
AIAA J. 18, 914*
1980. `
..59.2,44.3,61.0: three-D bubble - nice flow viz.*
WINKELMANN, A.E.; BARLOW, J. B.*
Flow field model for a rectangular planform wing beyond stall.*
AIAA J. 18, 1006*
1980. `
..24.4,18.2: large. 29 refs.*
POTTER, J. L.*
Review of the influence of cooled walls on boundary layer transition.*
AIAA J. 18, 1010*
1980. `
..28.3:*
CANTRELL, T.*
An 8088 processor for the S-100 bus, part I.*
BYTE vol. 5, no. 9, p. 46*
1980. `
..22.1:*
ROTT, N.*
Nonlinear acoustics - history and outlook (in German).*
Z. Flugwiss. 4, 185*
1980. `
..19.3,01.1: copious statistics*
TUNG, T.C.; ADRIAN, R.J.*
Higher order estimates of conditional eddies in isotropic turbulence.*
Phys. Fluids 23, 1469*
1980. `
..59.0: doesn't look too scruffy*
MOSS, W.D.; BAKER, S.*
Recirculating flows associated with two-dimensional steps.*
Aero. Quart.31, 151*
1980. `
..44.2,27.1*
CALVERT, W.J.; HERBERT, M.B.*
Inviscid-viscous interaction method to predict the blade-to-blade performance of axial compressors*
Aero. Quart. 31, 173*
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. `
..31.3:*
FACKRELL, J. E.*
A flame ionisation detector for measuring fluctuating concentration.*
J. Phys. E. 13, 888*
1980. `
..44.2:*
GREITZER, E.M.*
Review - axial compressor stall phenomena.*
J. Fluids Engg 102, 134*
1980. `
..31.1: noch einmal*
FREYMUTH, P.*
Review - A bibliography of thermal anemometry.*
J. Fluids Engg 102, 152*
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. `
..24.1:*
CLARK, J.A.; LAM KIT*
Shear layer transition and the sharp-edged orifice.*
J. Fluids Engg 102, 219*
1980. `
..47.2:*
HUANG, T.T.; GROVES, N.C.; BELT, G.*
Boundary-layer flow on an axisymmetric body with an inflected stern. *
David Taylor report DTNSRDC-80/064*
1980. `
..59.0:*
EATON, J. K.; JOHNSTON, J.P.*
Turbulent flow reattachment - an experimental study of the flow and structure behind a backward-facing step.*
Thermosciences Division, Stanford Univ.,Rept MD-39*
1980. `
..53.0: scruffy*
SUNDARASIVA RAO, B.N.*
An experimental study of the effects of moderate to strong longitudinal curvature on turbulent boundary layers.*
PhD Thesis, Indian Inst. of Science.*
1980. `
..25.6:*
GROTZBACH, G.*
Numerical simulation of turbulent liquid metal flows in plane channels and annuli.*
Karlsruhe Nuclear Res.Centre Rept KfK 2968*
1980. `
..48.0: straightforward*
EL TELBANY, M.M.M.; REYNOLDS, A.J.*
Velocity distributions in plane turbulent channel flows.*
J. Fluid Mech. 100, 1*
1980. `
..42.3:*
DEARDORFF, J. W.; WILLIS, G.E.; STOCKTON, B.H.*
Laboratory studies of the entrainment zone of a convectively mixed layer.*
J. Fluid Mech. 100, 41*
1980. `
..25.6: QMC*
LOVE, M.D.*
Subgrid modelling studies with Burgers' equation.*
J. Fluid Mech. 100, 87*
1980. `
..01.2,21.3:*
ANTONIA, R.A.; PHAN-THIEN, N.; CHAMBERS, A.J.*
Taylor's hypothesis and the probability density functions of temporal velocity and temperature derivatives in a turbulent flow.*
J. Fluid Mech. 100, 193*
1980. `
..31.1: useful - Stanford notes - but not wonderful*
WILLS, J.A.B.*
Hot-wire and hot-film anemometry.*
Nat. Maritime Inst. R 82 and Stanford Thermosci. IL-45*
1980. `
..10.0:*
FACKRELL, J.E.; ROBINS, A.G.*
Concentration fields associated with emissions from point sources in turbulent boundary layers. Part 2 - The effects of source size.*
CEGB Rept MM/MECH/TF264*
1980. `
..01.1,21.2:*
KEFFER, J.F.; KAWALL, J.G.*
Structural features of plane turbulent shear flows.*
AIAA paper XXXXXXX*
1980. `
..61.0:*
BEARMAN, P.W.*
Review - Bluff body flows applicable to vehicle aerodynamics.*
J. Fluids Engg 102, 265*
1980. `
..49.0:*
ASHJAEE, J.; JOHNSTON, J.P.*
Straight-walled, two-dimensional diffusers - transitory stall and peak pressure recovery.*
J. Fluids Engg 102, 275*
1980. `
..49.0:*
KAISER, K.F.; McDONALD, A.T.*
Effect of wake-type nonuniform inlet velocity profiles on first appreciable stall in plane-wall diffusers.*
J. Fluids Engg 102, 283*
1980. `
..59.0:*
KIM, J.; KLINE, S.J.; JOHNSTON, J.P.*
Investigation of a reattaching turbulent shear layer - flow over a backward-facing step.*
J. Fluids Engg 102, 302*
1980. `
..49.0:useful data for test case - spoilers etc*
STEVENS, S.J.; WILLIAMS, G.J.*
The influence of inlet conditions on the performance of annular diffusers.*
J. Fluids Engg 102, 357*
1980. `
..46.0,48.0,62.0:*
MARSTERS, G.F.*
Measurements in the flowfield of a linear array of rectangular nozzles.*
J. Aircraft 17, 774*
1980. `
..02.1:*
BANDYOPADHYAY, P.*
Large structure with a characteristic upstream interface in turbulent boundary layers.*
Phys. Fluids 23, 2326*
1980. `
..24.4: Gaster involved*
GAD-EL-HAK, M.; RILEY, J. J.*
Visualization study of turbulent spots.*
Flow Research Co. Rept Flow-RR-162, AD A086831 *
1980. `
..24.2:*
SMITH, F.T.; BODONYI, R.J.*
On the stability of the developing flow in a channel or circular pipe.*
Quart. J. Mech. Appl. Math. 33, 293*
1980. `
..24.1: Mixing layer - swept laser beam*
MENSING, P.; FIEDLER, H.*
On flow visualization in highly turbulent flow of high Reynolds numbers (in German).*
Z. Flugwiss. 4, 366*
1980. `
..31.1: min. volts when flow speed = flying wire speed*
LEHMANN, V.*
Uncalibrated rotating hot-wire probes for the measurement of small velocity vectors.*
Z. Flugwiss. 4, 369*
1980. `
..24.4: flow viz. - spiral vortices*
ACRIVLELLIS, M.*
Instabilities in the wall boundary layer of swirl flows.*
Z. Flugwiss. 4, 374*
1980. `
..50.0:*
BAUER, K.; STRAUB, J.; GRIGULL, U.*
Influence of free-stream turbulence intensity on heat transfer in the two-dimensional turbulent boundary layer of an accelerated compressible flow.*
Int. J. Heat Mass Transf. 23, 1635*
1980. `
..53.0: equals thesis*
GILLIS, J.C.; JOHNSTON, J.P.; MOFFAT, R.J.; KAYS, W.M.*
Turbulent boundary layer on a convex, curved surface.*
Stanford Univ. Thermosci. Div. Rept. HMT-31, NASA CR 3391*
1980. `
..31.2: large vel fluc and T contamination*
ANTONIA, R.A.; CHAMBERS, A.J.; HUSSAIN, A.K.M.F.*
Errors in simultaneous measurements of temperature and velocity in the outer part of a heated jet.*
Phys. Fluids 23, 871*
1980. `
..59.0: LDV mean flow only*
ARMALY, B.F.; DURST, F.; SCHOENUNG, B.*
Measurements and predictions of flow downstream of a two-dimensional single backward-facing step.*
Karlsruhe SFB 80/ET/172*
1980. `
..48.0:*
VAN DEN BERG, B.; OSKAM, B.*
Boundary layer measurements on a two-dimensional wing with flap and a comparison with calculations.*
NLR MP 79034 U and AGARD CP 271*
1980. `
..16.2:*
BERTELRUD, A.*
Local skin friction and static pressure on a swept wing in flight.*
AIAA-80-0423-CP*
1980. `
..27.2: Mechul and Hilbert*
CEBECI, T.; STEWARTSON, K.; WILLIAMS, P.G.*
Separation and reattachment near the leading edge of a thin airfoil at incidence.*
AGARD Conf. Proc. 291*
1980. `
..01.0,05.0: flow viz and hot wire*
FALCO, R.E.*
The production of turbulence near a wall.*
AIAA-80-1356*
1980. `
..23.0: not very impressive*
SCHEWE, G.*
On characteristic structures in time functions in turbulent surface pressure fluctuations*
Max Planck Inst. fur Stromungsforsch. -1/ 1980, N81-24399*
1980. `
..62.0:scruffy meas but demonstrates importance*
FOLEY, W.H.; FINLAY, D.B.*
Fountain jet turbulence*
AFOSR-TR-81-0286, AD-A098098*
1980. `
..60.0:interesting expt -just pitot and static at M=1.4,1.44,1.46*
KOOI, J.W.*
Influence of free stream Mach number on transonic shock wave boundary layer interaction*
VKI LS 1980-8*
1980. `
..53.0: Simon thesis - see ASME 81-HT-78*
SIMON, T.W.; MOFFAT, R.J.; JOHNSTON, J.P.; KAYS, W.M.*
Turbulent boundary layer heat transfer experiments - convex curvature effects including introduction and recovery*
Stanford Thermosci. Divn. Rept. HMT-32*
1980. `
..30.2: tunnel interference*
GOULD, R.W.F.*
Outline of Maskell's theory as applied to flat plates.*
Unpublished notes, Nat. Maritime Inst.*
1980. `
..50.0,44.2:*
HAH, C.; LAKSHMINARAYANA, B.*
Free-stream turbulence effects on the development of rotor wake.*
AIAA-80-1431*
1980. `
..44.2,45.0: further analysis of earlier L, N and H. work*
LANGSTON, L.S.*
Crossflows in a turbine cascade passage.*
J. Engg Power 102, 866*
1980. `
..27.1: 1980 version*
LOCK, R.C.*
A review of methods for predicting viscous effects on aerofoils and wings at transonic speeds.*
RAE Tech. Memo. Aero 1860, AGARD Conf. Proc. 291 *
1980. `
..30.1:*
NEISE, W.*
Noise and noise abatement in fans and blowers - a review.*
DFVLR-FB 80-16*
1980. `
..51.0,62.0: blames pressure - but this doesn't work in elliptic jets*
RODI, W.*
Explanation of three-dimensional wall jet spreading. *
AIAA J. (submitted) and see Prog. Aerosp. Sci. 19, 81, 1981*
1980. `
..59.2,27.1: Horton lives*
WILLIAMS, B.R.*
The prediction of the bursting of laminar separation bubbles in the design of two-dimensional high-lift aerofoils.*
RAE TR 80060*
1980. `
..24.1: yes indeed - single stream*
WYGNANSKI, I.; OSTER, D.; FIEDLER, H.*
A forced, plane, turbulent mixing-layer - a challenge for the predictor.*
Turbulent Shear Flows 2, Springer, Berlin, p. 314*
1980. `
..24.1: further meas., in two stream layer*
WYGNANSKI, I.; OSTER, D.*
The forced mixing layer between parallel streams.*
Tel-Aviv Univ. Rept.*
1980. `
..25.6:says Smag. is SGS mixing length*
YOSHIZAWA, A.*
A statistical investigation upon the Smagorinsky model in the large-eddy simulation of turbulence.*
J. Fluid Mech. (submitted)*
1980. `
..05.0: electrochemical - Hanratty man*
LAU, K.K.*
Study of turbulence structure close to a wall using conditional sampling techniques.*
Ph.D. thesis, University of Illinois-Urbana.*
1980. `
..31.3: 15kHz freq. response. PB has*
DIBBLE, R.W.; HOLLENBACH, R.E.*
Laser Rayleigh thermometry in turbulent flames.*
Sandia Corp. Rept. SAND80-8623 (presented at 18th Int. Sympo. on Combustion). *
1980. `
..25.7,25.10:quasi-time-dep MacCormack - chat on non-ortho mesh*
SELLS, C.C.L.*
Solution of the Euler equations for transonic flow past a lifting aerofoil*
RAE TR 80065*
1980. `
..25.5,27.1:synoptic of 79-1543, time-dep split implicit, non-ortho*
SHAMROTH, S.J.; GIBELING, H.J.*
Navier-Stokes solution of the turbulent flowfield about an isolated airfoil*
AIAA J. 18, 1409*
1980. `
..27.3:Univ. Coll. - matching, oblique coords. Finally like Ghia*
BARCLAY, W.H.; RIDHA, A.H.*
Flow in streamwise corners of arbitrary angle*
AIAA J. 18, 1413*
1980. `
..26.2,25.7:Ames, clever upwinding, num. coord. transformn., 3D*
HOLST, T.L.*
Fast, conservative algorithm for solving the transonic full-potential equation*
AIAA J. 18, 1431*
1980. `
..27.2: blunt base, simple turb model, M>1*
WASKIEWICZ, J. D.; SHANG, J. S.; HANKEY, W.L.*
Numerical simulation of near wakes utilizing a relaxation turbulence model*
AIAA J. 18, 1440*
1980. `
..24.1: discussion of lam vs turb initial BL*
HUSSAIN, A.K.M.F.; HUSAIN, Z.D.*
Turbulence structure in the axisymmetric free mixing layer*
AIAA J. 18, 1462*
1980. `
..61.0,60.0: horseshoe vortices*
KUSSOY, M.I.; VIEGAS, J. R.; HORSTMAN, C.C.*
Investigation of a three-dimensional shock wave separated turbulent boundary layer*
AIAA J. 18, 1477*
1980. `
..54.0: 1/72 scale in water tunnel...vortices from strake*
LORINCZ, D.J.*
Flow visualization study of the F-14 fighter aircraft configuration*
NASA CR 163098, N80-33350*
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. `
..27.1,26.2:Colorado Springs - TSP plus P.D. Smith lag ent.*
FIRMIN, M.C.P.*
Calculations of transonic flow over wing/body combinations with an allowance for viscous effects.*
RAE Tech Memo Aero 1861, AGARD Conf. Proc. 291*
1980. `
..24.4:intermittency, etc*
FRASER, C.J.; MILNE, J. S.*
Boundary layer development from transition provoking devices.*
Int. J. Heat and Fluid Flow 2, 165*
1980. `
..28.3:useful glossy book*
MORGAN, E.*
Microprocessors. A short introduction.*
Department of Industry.*
1980. `
..09.1: polymers, etc - 47 refs.*
GRANVILLE, P.S.*
Frictional drag reduction - a literature survey of progress from Spring 1979 to Spring 1980*
David Taylor NSRDC Rept. 80-SPD-569-07*
1980. `
..31.1: variable n and remarks on nasty yaw cal*
BRUUN, H.H.; TROPEA, C.*
Calibration of normal, inclined and X-array hot-wire probes*
Karlsruhe SFB 80/M/170*
1980. `
..27.1:includes his own scheme for using delstar as b.c. on both calcs*
LE BALLEUR, J.C.*
Computation of flows including strong viscous interactions with coupling methods*
AGARD Conf. Proc. 291*
1980. `
..53.0:energy bal and l(Rf)*
NAKAMURA, I.; YAMASHITA, S.; FURUYA, Y.*
Experiments on turbulence properties in the thick turbulent boundary layer on a rotating conical body of radius decresing towards downstream*
Turbulent Shear Flows 2 (Springer, Berlin) p. 99*
1980. `
..22.2: interesting selection *
DURST, F.; LAUNDER, B.E.; SCHMIDT, F.W.; WHITELAW, J.H. (Eds.)*
Turbulent Shear Flows 2*
Springer, Berlin*
1980. `
..27.1: excellent general review of his and others' work*
MELNIK, R.E.*
Turbulent interactions on airfoils at transonic speeds - recent developments*
AGARD Conf. Prof. 291 *
1980. `
..51.0:thesis, with hot wire meas of Re stress*
SARIPALLI, K.R.; SIMPSON, R.L.*
Investigation of blown boundary layers with an improved wall jet system*
NASA CR 3340*
1980. `
..30.2:Ames 12 ft and Langley 8ft (no screens - worse) - both poor near M=1*
HARVEY, W.D.; STAINBACK, P.C.; OWEN, F.K.*
Evaluation of flow quality in two large NASA wind tunnels at transonic speeds*
NASA TP 1737 and J. Aircraft 18, 451, 1981*
1980. `
..10.0:*
CHEN, C.J.; RODI, W.*
Vertical turbulent buoyant jets - a review of experimental data.*
Pergamon Press, Oxford.*
1980. `
..59.0,11.3:*
OTA, T.; KON, N.*
Turbulent transfer of momentum and heat in a separated and rear attached flow over a blunt flat plate.*
J. Heat Transf. 102, 749*
1980. `
..11.3:just so*
ANDREOPOULOS, J.; BRADSHAW,P.*
The thermal boundary layer far downstream of a spanwise line source of heat.*
J. Heat Transf. 102, 755*
1980. `
..24.1: just so*
ZAMAN, K.B.M.Q.; HUSSAIN, A.K.M.F.*
Vortex pairing in a circular jet under controlled excitation.*
Parts I and II, J. Fluid Mech. 101, 449*
1980. `
..42.2:*
THORPE, S.A.; HALL, A.J.*
The mixing layer of Loch Ness.*
J. Fluid Mech. 101, 687*
1980. `
..11.3*
TALBOT, L.; CHENG, R.K.; SCHEFER, R.W.; WILLIS, D.R.*
Thermophoresis of particles in a heated boundary layer.*
J. Fluid Mech. 101, 737*
1980. `
..01.2,11.2:*
SREENIVASAN, K.R.; TAVOULARIS, S.*
On the skewness of the temperature derivatives in turbulent flows.*
J. Fluid Mech. 101, 783*
1980. `
..24.4:conf proc - in Aero Lib*
EPPLER, R.; FASEL, H.*
Laminar-turbulent transition.*
Springer-Verlag, Berlin, ISBN 3-540-10142*
1980. `
..62.0:*
TYLER, R.A.; WILLIAMSON, R.G.*
Confined mixing of coaxial flows.*
Canadian NRC Rept LR/602*
1980. `
..59.2: Maskell-like*
ORLOFF, K.L.*
Spanwise lift distribution on a wing from flow field velocity surveys.*
J. Aircraft 17, 75*
1980. `
..31.1: papers on LDA and HWA*
ANON.*
Various papers*
DISA Information no. 25*
1980. `
..31.3: small scale high order moments*
PARK, J.T.; VAN ATTA, C.W.*
Hot- and cold-wire sensitivity corrections for moments of the fine scale turbulence in heated flows.*
Phys. Fluids 23, 701*
1980. `
..31.1: not very realistic - wire length dominates*
VAGT, J.D.; FERNHOLZ, H.H.*
A discussion of probe effects and improved measuring techniques in the near wall region of an incompressible three-dimensional turbulent boundary layer.*
AGARD CP 271*
1980. `
..31.1:*
FREYMUTH, P.*
Sine-wave testing of non-cylindrical hot-film anemometers according to the Bellhouse-Schultz model.*
J. Phys. E. 13, 98*
1980. `
..31.1:*
SMITS, A.J.; PERRY, A.E.*
The effect of varying resistance ratio on the behaviour of constant- temperature hot-wire anemometers.*
J. Phys. E. 13, 451*
1980. `
..31.1:*
HUFFMAN, G.D.*
Calibration of triaxial hot-wire probes using a numerical search algorithm.*
J. Phys. E. 13, 1177*
1980. `
..31.1:*
COMTE-BELLOT, G.*
Experimental methods and techniques in turbulence research.*
AGARD CP 271*
1980. `
..31.2:*
TORKELSSON, S.A.*
A new type of resistance thermometer for accurate temperature measurement in high gradient thermal boundary layers.*
J. Phys. E. 13, 549*
1980. `
..31.3:*
ANON.*
Testing and measurement techniques in heat transfer and combustion.*
AGARD Conf. Proc. 281*
1980. `
..30.2: very old expts - n=13 and Re,trans up to 6 million*
WINTER, K.G.; MASKELL, E.C.*
The Reynolds number for transition on a flat plate in the RAE 4ft x 3ft low turbulence wind tunnel*
RAE TM Aero 1854*
1980. `
..13.0: just so*
HANJALIC, K.; LAUNDER, B.E.*
Sensitizing the dissipation equation to irrotational strains*
J. Fluids Engg 102, 34*
1980. `
..60.0,27.2: triple deck for shock - see Inger in same Proc*
STANEWSKY, E.; NANDANAN, M.; INGER, G.R.*
Coupling of a shock boundary layer interaction module with a viscous inviscid computation method*
AGARD Conf. Proc. 291*
1980. `
..27.2: in French*
LE BALLEUR, J.C.; NERON, M.*
Calculation of separated viscous flows on aerofoils by a coupling approach*
AGARD Conf. Proc. 291*
1980. `
..41.0: PR document*
KLINE, S.J.*
The 1980-81 AFOSR-HTTM-Stanford conference on complex turbulent flows - comparison of computation and experiment*
AGARD Conf. Prof. 291*
1980. `
..27.4: MAVIS - somewhat optimistic*
BUTTER, D.J.; WILLIAMS, B.R.*
The development and application of a method the viscous flow about high lift aerofoils*
AGARD Conf. Proc. 291*
1980. `
..27.1.27.2: see refs to individual papers*
ANON.*
Computation of viscous-inviscid interactions*
AGARD-CP-291*
1980. `
..17.1,15.0: alg. eddy vis was OK for 18 percent, even in recirc region*
MARVIN, J.G.; LEVY, L.L.; SEEGMILLER, H.L.*
Turbulence modeling for unsteady transonic flows*
AIAA J. 18, 489*
1980. `
..60.0:sep. length increases strongly with M and Te*
PADOVA, C.; FALK, T.J.; WITTLIFF, C.E.*
Experimental investigation of similitude parameters governing transonic shock-boundary layer interactions*
AIAA-80-0158*
1980. `
..25.7,60.0:different power laws for nl. and tgtl. profiles*
PAYNTER, G.C.*
Analysis of multiple weak glancing shock boundary layer interactions*
AIAA-80-0196*
1980. `
..60.0: backstep and ramp to get self-pres ML before reatt.*
SETTLES, G.S.; BACA, B.K.; WILLIAMS, D.R.; BOGDONOFF, S.M.*
A study of reattachment of a free shear layer in compressible turbulent flow*
AIAA-80-1408*
1980. `
..53.1:calcs and meas of all Reynolds stresses*
NAKAMURA, I.; YAMASHITA, S.; YAMAMOTO, K.*
On the turbulent boundary layer on a spinning tail body in an axial flow*
Mem. Fac. Engg, Nagoya Univ., 32, 282*
1980. `
..13.0:Launder's Davis team, inc. Durst on lasers*
KOLLMANN, W. (Ed.)*
Measurements and predictions of complex turbulent flows*
VKI Lecture Series 1980-3*
1980. `
..59.3,61.0:sums up Pailhas thesis etc - PB has*
COUSTEIX, J.; PAILHAS, G.*
Measurements of mean velocity and Reynolds stress tensor within a wake of a swept wing*
ONERA Rept. OA 41/2259 AYD (DERAT 25/5004 DY) *
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. `
..11.6,24.1:schlieren pics showing orderly structure behind step*
GANJI, A.R.; SAWYER, R.F.*
Experimental study of the flowfield of a two-dimensional premixed turbulent flame*
AIAA J. 18, 817*
1980. `
..11.6,24.1: much chat about ML structure - see AIAA J. 18, 817*
GANJI, A.T.; SAWYER, R.F.*
Turbulence, combustion, pollutant and stability characterization of a premixed, step combustor*
NASA CR 3230*
1980. `
..25.8:one of a series - from Keith U.*
MITCHELL, A.R.; GRIFFITHS, D.F.*
Upwinding by Petrov Galerkin methods in convection diffusion problems*
J. Comp. Appl. Math. 6, 219*
1980. `
..16.1:log laws OK for small angle, nothing good for large angle*
PIERCE, F.J.; McALLISTER, J.E.*
Near wall similarity in a pressure driven three dimensional turbulent boundary layer*
VPI-E-80-32*
1980. `
..54.0,62.0: applied but interesting*
ALMOSNINO, D.; ROM, J.*
Alleviation of the lateral forces and moments acting on a slender body at high angles of attack, using jet injection at subsonic and transonic speeds*
A-80-1558-CP, in AIAA CP806*
1980. `
..22.2: pretty good*
ZINSSER, W.*
On writing well*
Harper and Row, ISBN 0-06-047396-7*
1980. `
..13.0,41.1: hint, but no more, of zonal modelling*
NIELSEN, J.C.*
Missile aerodynamics - past, present, future*
J. Spacecraft and Rockets, 17, 165*
1980. `
..13.0, 53.0: sort of linearized, RDT etc but gets fiddle factor = 10*
BERTOGLIO, J.P.; CHARNAY, G.; MATHIEU, J.*
Effects of rotation on a turbulent shear flow - application to the case of turbomachines*
J. de Mec. Applique 4, 421*
1980. `
..24.1: 3-d and centered off the jet axis*
TSO, J.; KOVASZNAY, L.S.G.; HUSSAIN, A.K.M.F.*
Search for large scale coherent structures in the nearly self preserving region of the axisymmetric turbulent jet*
AIAA paper 80-1355*
1980. `
..25.5,62.0: k, eps. - 20 x 15 x 15*
JONES, W.P.; MCGUIRK, J.J.*
Computation of a round turbulent jet discharging into a confined crossflow*
Turbulent Shear Flows 2 (Ed. L.J.S. Bradbury et al., Springer), p. 233*
1980. `
..27.1,59.2:crude modules but a real working program*
EPPLER, R.; SOMERS, D.M.*
A computer program for the design and analysis of low speed airfoils*
NACA TM 80210*
1980. `
..24.7: just so*
LEONARD, A.*
Review. Vortex methods for flow simulation*
J. Comp. Phys. 37, 289*
1980. `
..13.0: just so*
LAUNDER, B.E.*
Reynolds stress closures - status and prospects*
AGARD CP 271*
1980. `
..28.1,28.2: approx Aero II Elec Engg syllabus*
VASSOS, B.H.; EWING, G.W.*
Analog and digital electronics for scientists*
Wiley*
1980. `
..54.0,21.1: normal stresses only*
HABIB, M.A.; WHITELAW, J.H.*
Velocity characteristics of confined coaxial jets with and without swirl*
J. F1uids Engg 102, 47*
1980. `
..24.1: not much difference*
BROWAND, F.K.; LATIGO, B.O.*
The growth of the two dimensional mixing layer from a turbulent and non-turbulent boundary layer*
Phys. Fluids 22, 1011*
1980. `
..50.0: Orr-Somm.-like equation for Wiener-Hermite expansion - agrees with Hunt and Graham*
KAMBE, R.; DOI, M.; IMAMURA, T.*
Turbulent flows near flat plates*
J. Phys. Soc. Japan 49, 763*
1980. `
..31.1: substrate effects on conical probe in water*
LUECK, R.G.*
The calibration of a hot film turbulence probe*
J. Geophys. Res. 85, 4923*
1980. `
..24.2:stag. flow versus Taylor-Gortler*
DALLMANN, U.*
Stability of three dimensional shear flows - criteria for inviscid disturbance excitation*
DFVLR-FB 80-05*
1980. `
..59.4,45.0,54.0: NACA 0012 with square and semicircular tips - incidence not meaningful*
AUTHOR*
TITLE*
NASA CR 3281*
1980. `
..21.2,19.2:Re, lambda up to 1000 - local isotropy assumed*
ANTONIA, R.A.; SATYAPRAKASH, B.R.; HUSSAIN, A.K.M.F.*
Measurements of dissipation rate and some other characteristics of turbulent plane and circular jets*
Phys. Fluids 23, 695*
1980. `
..50.0: separates effects of intensity and length scale*
HANCOCK, P.E.*
The effect of free-stream turbulence on turbulent boundary layers*
PhD Thesis, Imperial College, London*
1980. `
..14.0,13.0,15.0: just so - 3-chapter book, 100 pages, 200 refs., chapter on hydraulics examples*
RODI, W.*
Turbulence models and their application in hydraulics*
Int. Assoc. for Hydraulic Res., Delft, Netherlands*
1980. `
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