..43.0,21.3:*
DUNCAN, R.L.*
An experimental investigation of Taylor's hypothesis for atmospheric boundary layer flow.*
NASA TM-X-61902*
1969. `
..48.0,21.2:*
CHAMPAGNE, F.H.; WYGNANSKI, I.J.*
Coaxial turbulent jets.*
Boeing Sci. Res. Lab. D1-82-0958*
1970. `
..48.0,21.2:*
HESKESTAD, G.*
Measurements in a two-dimensional turbulent jet.*
J. Appl. Mech. 32, 721*
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. `
..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. `
..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. `
..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. `
..13.0,21.2: vertical strain*
POPE, S.B.*
An explanation of the turbulent round-jet / plane-jet anomaly*
AIAA J. 16, 279*
1978. `
..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. `
..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. `
..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. `
..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. `
..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. `
..01.1,21.2:*
KEFFER, J.F.; KAWALL, J.G.*
Structural features of plane turbulent shear flows.*
AIAA paper XXXXXXX*
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. `
..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. `
..24.1,21.3: refers to Wills*
HUSSAIN, A.K.M.F.; CLARK, A.R.*
Measurements of wavenumber-celerity spectrum in plane and axisymmetric jets.*
AIAA J. 19, 51*
1981. `
..21.3: only at ystar=70*
McCONACHIE, P.J.*
The distribution of convection velocities in turbulent pipe flow*
J. Fluid Mech. 103, 65*
1981. `
..21.3: seems not to have read Wills on U(k, omega)*
GOLDSCHMIDT, V.W.; YOUNG, M.F.; OTT, E.S.*
Turbulent convective velocities (broadband and wavenumber dependent) in a plane jet*
J. Fluid Mech. 105, 327*
1981. `
..24.1,21.2: at last*
GOLDSCHMIDT, V.W.; BRADSHAW, P.*
Effects of nozzle exit turbulence on the spreading (or widening) rate of plane free jets*
ASME paper 81-FE-22*
1981. `
..43.0,21.3: conv. vel = U for ky .gt. 3, iso only for ky .gt. 20*
WEBSTER, I.T.; BURLING, R.W.*
A test of isotropy and Taylor's hypothesis in the atmospheric boundary layer*
Boundary-Layer Met. 20, 429*
1981. `
..21.1:calcs, showing viscous stress gts significant in entrainment flow*
SCHNEIDER, W.*
Flow induced by jets and plumes*
J. Fluid Mech. 108, 55*
1981. `
..21.2: self-pres now*
CERVANTES de GORTARI, J.; GOLDSCHMIDT, V.W.*
The apparent flapping motion of a turbulent plane jet - further experimental results*
J. Fluids Engg 103, 119*
1981. `
..21.3,24.1:T's H works if you use large eddy bulk vel*
ZAMAN, K.B.M.Q.; HUSSAIN, A.K.M.F.*
Taylor hypothesis and large scale coherent structures*
J. Fluid Mech. 112, 379*
1981. `
..21.2:momentum nearly conserved - Schlichting soln is OK*
RANKIN, G.W.; SRIDHAR, K.; ARULRAJA, M.; KUMAR, K.R.*
An experimental investigation of laminar axisymmetric submerged jets*
J. Fluid Mech. 133, 217*
1983. `
..21.2:alternating large eddies, not true flapping*
ANTONIA, R.A.; BROWNE, L.W.B.; RAJAGOPALAN, S.; CHAMBERS, A.J.*
On the organized motion of a turbulent plane jet*
J. Fluid Mech. 134, 49*
1983. `
..11.2,19.2,21.2: temp. var. eqn*
ANTONIA, R.A.; BROWNE, L.W.B.*
The destruction of temperature fluctuations in a turbulent plane jet*
J. Fluid Mech. 134, 67*
1983. `
..24.1,21.2: persistence of initial conditions*
GUTMARK, E.; HO, C.M.*
Preferred modes and the spreading rates of jets*
Phys. Fluids 26, 2932*
1983. `
..48.0,21.2,11.3: simple vel. and temp fluctuations*
BROWNE, L.W.B.; ANTONIA, R.A.; RAJAGOPALAN, S.; CHAMBERS, A.J.*
Interaction region of a two-dimensional turbulent plane jet in still air*
Structure of Complex Turbulent Shear Flow (R. Dumas and L. Fulachier, Eds.) Springer, p. 411*
1983. `
..11.3,21.0: good crosscheck of dissipation*
ANTONIA, R.A.; BROWNE, L.W.B.; CHAMBERS, A.J.; RAJAGOPALAN, S.*
Budget of the temperature variance in a turbulent plane jet*
Int. J. Heat Mass Transf. 26, 41*
1983. `
..11.2,19.2,21.3:correction to T's H do not seem warranted*
BROWNE, L.W.B.; ANTONIA, R.A.; RAJAGOPALAN, S.*
The spatial derivative of temperature in a turbulent flow and Taylor's hypothesis*
Phys. Fluids 26, 1222*
1983. `
..21.2:momentum nearly conserved - Schlichting soln is OK*
RANKIN, G.W.; SRIDHAR, K.; ARULRAJA, M.; KUMAR, K.R.*
An experimental investigation of laminar axisymmetric submerged jets*
J. Fluid Mech. 133, 217*
1983. `
..21.2:alternating large eddies, not true flapping*
ANTONIA, R.A.; BROWNE, L.W.B.; RAJAGOPALAN, S.; CHAMBERS, A.J.*
On the organized motion of a turbulent plane jet*
J. Fluid Mech. 134, 49*
1983. `
..11.2,19.2,21.2: temp. var. eqn*
ANTONIA, R.A.; BROWNE, L.W.B.*
The destruction of temperature fluctuations in a turbulent plane jet*
J. Fluid Mech. 134, 67*
1983. `
..24.1,21.2: persistence of initial conditions*
GUTMARK, E.; HO, C.M.*
Preferred modes and the spreading rates of jets*
Phys. Fluids 26, 2932*
1983. `
..48.0,21.2,11.3: simple vel. and temp fluctuations*
BROWNE, L.W.B.; ANTONIA, R.A.; RAJAGOPALAN, S.; CHAMBERS, A.J.*
Interaction region of a two-dimensional turbulent plane jet in still air*
Structure of Complex Turbulent Shear Flow (R. Dumas and L. Fulachier, Eds.) Springer, p. 411*
1983. `
..11.3,21.0: good crosscheck of dissipation*
ANTONIA, R.A.; BROWNE, L.W.B.; CHAMBERS, A.J.; RAJAGOPALAN, S.*
Budget of the temperature variance in a turbulent plane jet*
Int. J. Heat Mass Transf. 26, 41*
1983. `
..11.2,19.2,21.3:correction to T's H do not seem warranted*
BROWNE, L.W.B.; ANTONIA, R.A.; RAJAGOPALAN, S.*
The spatial derivative of temperature in a turbulent flow and Taylor's hypothesis*
Phys. Fluids 26, 1222*
1983. `
..62.0,21.2,46.0: rect jet alone and near circular jet*
BAKER, J.N.*
The flow development in a shielding jet*
Aero. J. 88, 435*
1984. `
..21.1,18.1: very hot jet*
BICKNELL, G.V.*
A model for the surface brightness of a turbulent low Mach number jet. I and II*
Unpublished papers, Mt Stromlo and Siding Spring Obs. *
1984. `
..19.3,21.2: higher order moments diverge from log normal expectation*
ANSELMET, F.; GAGNE, Y.; HOPFINGER, E.J.; ANTONIA, R.A.*
High order velocity structure functions in turbulence shear flows*
J. Fluid Mech. 140, 63*
1984. `
..21.3: Taylor's hyp more or less OK*
ANTONIA, R.A.; BROWNE, L.W.B.; BRITZ, D.; CHAMBERS, A.J.*
A comparison of properties of temporal and spatial temperature increments in a turbulent plane jet*
Phys. Fluids 27, 87*
1984. `
..24.1,21.2: correln meas. say its 3D*
OLER, J.W.; GOLDSCHMIDT, V.W.*
Coherent structures in the similarity region of two-dimensional turbulent jets*
J. Fluids Engg. 106, 187*
1984. `
..21.2: circular with free stream - initial results*
TATAR, T.G.; STOCK, D.E.*
Measurements in a circular two-dimensional self-preserving turbulent jet*
Presented at Ninth Symposium on Turbulence, Rolla*
1984. `
..24.1,21.2: mucky base vortices as well as coherent structure*
KO, N.W.M.; LAM, K.M.*
Further measurements in the initial region of an annular jet*
J. Sound Vib. 92, 333*
1984. `
..48.0,21.2: orderly structures in phase in the two mixing layers - superposition no go*
BROWNE, L.W.B.; ANTONIA, R.A.; CHAMBERS, A.J.*
The interaction region of a turbulent plane jet*
J. Fluid Mech. 149, 355*
1984. `
..24.1,21.2:chamfered nozzles*
KIBENS, V.*
Control of jet flowfield dynamics*
MDC-Q1214, AD=A143 631*
1984. `
..21.2,24.1:flapping increases with x - real*
ANTONIA, R.A.; CHAMBERS, A.J.; BROWNE, L.W.B.; RAJAGOPALAN, S.*
The organized structure in a slightly heated turbulent plane jet*
Turbulence and Chaotic Phenomena in Fluids (T. Tatsumi, Ed.) North-Holland, p.529*
1984. `
..21.1,24.1: hexagonal rotating gizmos, large x/d*
BERNAL, L.; SAROHIA, V.*
Large amplitude forcing of a high speed two-dimensional jet*
JPL Pub. 84-91*
1984. `
..21.2,32.2,24.1: some info on technique*
KOMPENHANS, J.; HOFER, H.R.; RANNENBERG, S.*
Untersuchung von Dichtegradientenschwankungen in einem turbulenten Freistrahl mit Hilfe der Laser Schlieren Kreuzstrahl Methode*
DFVLR-FB 85-19*
1985. `
..21.2:because of impeded entrainment - see also p. 111*
SCHNEIDER, W.*
Decay of momentum flux in submerged jets*
J. Fluid Mech. 154, 91*
1985. `
..21.2,42.2: nozzle span vertical - tends to flatulence*
GIGER, M.; JIRKA, G.H.; DRACOS, T.*
Meandering jets in a shallow fluid layer*
Presented at 5th Symposium on Turbulent Shear Flows, Cornell, p. 7-23 (not in Proc.)*
1985. `
..11.3,21.2: coherent and random contributions to fluxes are roughly equal*
ANTONIA, R.A.; BRITZ, D.; CHAMBERS, A.J.*
Similarity between velocity and temperature fields in a turbulent plane jet*
Presented at 5th Symposium on Turbulent Shear Flows, Cornell, p. 14-l*
1985. `
..21.1,14.0: showing singularity at edge*
PAULLAY, A.J.; MELNIK, R.E.; RUBEL, A,; RUDMAN, S.; SICLARI, M.J.*
Similarity solutions for plane and radial jets using a k-e turbulence model*
ASME J. Fluids Engg 107, 79*
1985. `
..21.2,32.1: painstaking - LDV values lower than HWA*
RAMAPRIAN, B.R.; CHANDRASEKHARA, M.S.*
LDA measurements in plane turbulent jets*
J. Fluids Engg 107, 264*
1985. `
..21.2,62.0: Str up to 0.0048 - the jet flaps*
LAI, J.C.S.; SIMMONS, J.M.*
Instantaneous velocity measurements in a vane-excited plane jet*
AIAA J. 23, 1157*
1985. `
..24.1,21.1: Re=7600 so symmetrical structures*
CHAMBERS, A.J.; ANTONIA, R.A.; BROWNE, L.W.B.*
Effect of symmetry and asymmetry of turbulent structures on the intersction region of a plane jet*
Expts. in Fluids 3, 343*
1985. `
..21.1,24.1: scattered Re/initial effects - transition or Kotsovinos*
LEMIEUX, G.P.; OOSTUIZEN, P.H.*
Experimental study of the behaviour of plane turbulent jets at low Reynolds number*
AIAA J. 23, 1845*
1985. `
..24.1,21.2: disturbances symmetric then antisymmetric then swept*
THOMAS, F.O.; GOLDSCHMIDT, V.W.*
Structural characteristics of a developing turbulent planar jet*
J. Fluid Mech. 163, 227*
1986. `
..21.2,21.3,24.1: correlation maps - small spanwise length scales*
THOMAS, F.O.; BREHOB, E.G.*
An investigation of large scale structure in the similarity region of a two-dimensional turbulent jet*
Phys. Fluids 29, 1788*
1986. `
..11.6,21.0: turbulence reduced in jet combustion zone, increased downstream*
SISLAN, J.P.; JIANG, L.-Y.; CUSWORTH, R.A.*
Laser doppler velocimetry investigation of the turbulence structure of axisymmetric diffusion flames*
UTIAS Report No. 291*
1986. `
..24.1,21.0: a few turbulence measurements in transition*
TUCKER, H.J.; ISLAM, S.M.N.*
Development of axisymmetric laminar to turbulent free jets from initially parabolic profiles*
J. Fluids Engg 108, 321*
1986. `
..21.0,24.1,22.1: symmetric structures*
THOMAS, F.O.; GOLDSCHMIDT, V.W.*
Acoustically induced enhancement of widening and fluctuation intensity in a two-dimensional turbulent jet*
J. Fluids Engg 108, 331*
1986. `
..21.0,24.1: extensive correlation maps*
ANTONIA, R.A.; CHAMBERS, A.J.; BRITZ, D.; BROWNE, L.W.B.*
Organised structures in a turbulent plane jet - topology and contribution to momentum and heat transport*
J. Fluid Mech. 172, 211*
1986. `
..24.1,21.0,46.0: non-circular orifices, especially with sharp corners, enhance mixing*
GUTMARK, E.; WYGNANSKI, I.*
Small scale mixing in the initial region of a jet*
Final Research Report - AD-A193-500*
1986. `
..23.0,21.3: low convection velocity, especially at low k (effect of backoff transducer?)*
McGRATH, B.E.; SIMPSON, R.L.*
Some features of surface pressure fluctuations in turbulent boundary layers with zero and favorable pressure gradients*
NASA CR 4051*
1987. `
..21.1,54.0: includes vw - says swirl decreases mixing at large x*
ELSNER, J.W.; KURZAK, L.*
Characteristics of turbulent flow in slightly heated free swirling jets*
J. Fluid Mech. 180, 147*
1987. `
..21.0: turbulent flow would be similar*
SCHNEIDER, W.; ZAUNER, E.; BOHM, H.*
The recirculatory flow induced by a laminar axisymmetric jet issuing from a wall*
J. Fluids Engg 109, 237*
1987. `
..21.2: LIF in far field*
DAHM, W.J.A.; DIMOTAKIS, P.E.*
Measurements of entrainment and mixing in turbulent jets*
AIAA J. 25, 1216*
1987. `
..01.2,02.2,21.1: max conc near r = 0 . 13 x*
SHLIEN, D.J.*
Observations of dispersion of entrained fluid in the self-preserving region of a turbulent jet*
J. Fluid Mech. 183, 163*
1987. `
..21.2: HWA and LDV in far field to evaluate balances*
TAULBEE, D.B.; HUSSEIN, H.; CAPP, S.*
The round jet - experiment and inferences on turbulence modeling*
Presented at 6th Symposium on Turbulent Shear Flow, Toulouse, paper no. 10-5*
1987. `
..21.3,01.1,25.6: mainly eduction of circulation in x-y plane*
HUSSAIN, A.K.M.F.; JEONG, J.; KIM, J.*
Structure of turbulent shear flows*
Studying turbulence using numerical simulation databases, Ames/Stanford CTR-S87, p. 273*
1987. `
..21.0,11.2: temperature rise 100 deg C - Re effects on length scale*
OTUGEN, M.V.; NAMER, I.*
Rayleigh scattering temperature measurements in a plane turbulent air jet at moderate Reynolds numbers*
Expts. in Fluids 6, 461*
1988. `
..21.0,03.0: Re effects up to 7000 at least*
NAMER, I.; OTUGEN, M.V.*
Velocity measurements in a plane turbulent air jet at moderate Reynolds numbers*
Expts. in Fluids 6, 6*
1988. `
..21.0,54.0: just so (5-hole probe). S up to 0.49*
SAMET, M.; EINAV, S.*
Mean value measurements of a turbulent swirling-jet*
AIAA J. 26, 619*
1988. `
..10.0,42.3,21.1:  axial and radial vel. and dye conc.; Re no more than 1000*
PAPANICOLAOU, P.N.; LIST, E.J.*
Investigations of round vertical turbulent buoyant jets*
J. Fluid Mech. 195, 341*
1988. `
..22.1,21.0: supersonic flow - howling?*
ABDEL-FATTAH, A.M.; FAVALORO, S.C.*
Duct resonance and its effect on the performance of high-pressure ratio axisymmetric ejectors*
AIAA J. 26, 791*
1988. `
..24.1,21.0: specific, general and universal similarity*
DOWLING, D.R.*
Mixing in gas phase turbulent jets*
PhD Thesis, GALCIT*
1988. `
..18.1,18.2,21.2: density 0.64 of ambient - useful discussion of magnitudes of density fluctuations and Favre averaging*
SO, R.M.C.; ZHU, J.Y.; OTUGEN, M.V.; HWANG, B.C.*
Some measurements in a binary gas jet*
Arizona State University paper*
1989. `
..24.1,21.2,53.0: Reynolds stress measurements and misc. theory*
MASUDA, W.; ANDOH, S.*
Effects of curvature on the initial mixing region of a two-dimensional jet*
AIAA J. 27, 52*
1989. `
..21.3: uses Kim, Moin, Moser duct - works better than experiments suggest*
PIOMELLI, U.; BALINT, J.-L.; WALLACE, J.M.*
On the validity of Taylor's hypothesis for wall-bounded flows*
Phys. Fluids A1, 609*
1989. `
..11.6, 21.0: axial forcing - even the highly-3D flow is periodic*
STRAWA, A.W.; CANTWELL, B.J.*
Investigation of an excited jet diffusion flame at elevated pressure*
J. Fluid Mech. 200, 309*
1989. `
..21.2,46.0: instability analysis*
KOSHIGOE, S.; GUTMARK, E.; SCHADOW, K.C.; TUBIS, A.*
Initial development of noncircular jets leading to axis switching*
AIAA J. 27, 411*
1989. `
..21.2,54.0: solid-body rotation well behaved, free vortex on verge of breakdown at swirl no. of 0 . 48 (classical value 0 . 6)*
FAROKHI, S.; TAGHAVI, R.; RICE, E.J.*
Effect of initial swirl distribution on the evolution of a turbulent jet*
AIAA J. 27, 700*
1989. `
..21.2,53.0,62.0: bent-over jet in small crossflow - substantial net increase in entrainment etc.*
HANIU, H.; RAMAPRIAN, B.R.*
Studies on two-dimensional curved nonbuoyant jets in cross flow*
J. Fluids Engg 111, 78*
1989. `
..31.1,21.3: u-wire rotating in y-z plane - Taylor's hypothesis works*
SIRIVAT, A.*
Measurement and interpretation of space-time correlation functions and derivative statistics from a rotating hot wire in a grid turbulence*
Expts. in Fluids 7, 361*
1989. `
..21.2,53.0: results include intermittency and stress balance*
MASUDA, W.; ANDOH, S.*
Turbulence structure in an initial mixing region of a two-dimensional curved jet*
AIAA J. 27, 1038*
1989. `
..21.0,24.1: increased spreading rate for low freq. only - obviously passive*
BADRINARAYANAN, M.*
Excitation of plane jet by twin-vane oscillator*
AIAA 89-0663*
1989. `
..13.0,21.1: transport equations for time scale from k, eps. and Monte Carlo solution of Langevin model implying Rotta-like return to isotropy*
ANAND, M.S.; POPE, S.B.; MONGIA, H.C.*
Calculations of axisymmetric turbulent jets by the pdf method*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..11.2,21.2: yes, measurements, in co-flowing jet - LIF*
DAHM, W.J.A.; BUCH, K.A.*
High resolution three-dimensional (256^3) spatio-temporal measurements of the conserved scalar field in turbulent shear flows*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..11.2,21.2: Rayleigh scattering - effects are large*
KERSTEIN, A.R.; ET AL.*
Measurement and computation of differential molecular diffusion in a turbulent jet*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..54.0,21.2,13.0: stress equation better than k, eps.*
ABD AL-MASSEEH, W.A., BRADLEY, D.; GASKELL, P.H.; LAU, A.K.C.*
The numerical predictability of strongly swirling flows*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..31.1,21.2: not locally iso at Re = 90000*
HUSSEIN, H.J.; GEORGE, W.K.*
Measurement of small scale turbulence in an axisymmetric jet using moving hot-wires*
7th Sympo. on Turbulent Shear Flows, Stanford Univ.*
1989. `
..24.1,21.2: rich behavior - slot Reynolds number 8000*
THOMAS, F.O.; CHU, H.C.*
An experimental investigation of the transition of a planar jet - subharmonic suppression and upstream feedback*
Phys. Fluids A1, 1566*
1989. `
..21.0,02.1: reversal is rare and usually confined to non-turbulent zones*
CHUA, L.P.; ANTONIA, R.A.*
Flow reversal and intermittency of a turbulent jet*
AIAA J. 27, 1494*
1989. `
..21.2,17.1: interesting approach to steady state*
SEN, M.; HERNANDEZ, J.; CERVANTES, J.G.*
Longitudinal and transverse dimensions of an incipient jet generated by a constant head*
Expts. in Fluids 8, 107*
1989. `
..24.1,21.2: not just transition - Titan plume*
MUNGAL, M.G.; HOLLINGSWORTH, D.K.*
Organized motion in a very high Reynolds number jet*
Phys. Fluids A1, 1615*
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. `
..46.0,21.2: aspect ratio 5 - see also recent Hussain. No uw or vw*
QUINN, W.R.*
On mixing in an elliptic turbulent free jet*
Phys. Fluids A1, 1716*
1989. `
..24.1,21.0: quite similar to plane wake*
THOMAS, F.O.*
An experimental investigation into the role of simultaneous amplitude and phase modulation in the transition of a planar jet*
Phys. Fluids A2, 553*
1990. `
..23.0,21.3: Re too low for 1/k spectrum*
CHOI, H.; MOIN, P.*
On the space-time characteristics of wall-pressure fluctuations*
Phys.  Fluids A2, 1450*
1990. `
..21.0: Re only 16000 -- complicated stress profiles*
GLADNICK, P.G.; ENOTIADIS, A.C.; LARUE, J.C.; SAMUELSEN, G.S.*
Near-field characteristics of a turbulent coflowing jet*
AIAA J. 28, 1405*
1990. `
..11.6,21.1: molecular diffusion plus randomly-occurring spatial rearrangements.  Parts 1 and 2 in combustion journals*
KERSTEIN, A.R.*
Linear-eddy modelling of turbulent transport.  Part 3.  Mixing and differential molecular diffusion in round jets*
J. Fluid Mech. 216, 411*
1990. `
..21.2,11.6,24.1: Re up to 20000, LIF for conc. - find large eddies*
DAHM, W.J.A.; DIMOTAKIS, P.E.*
Mixing at large Schmidt number in the self-similar far field of turbulent jets*
J. Fluid Mech. 217, 299*
1990. `
..24.1,21.2: low Re - up to 40000*
DOWLING, D.R.; DIMOTAKIS, P.E.*
Similarity of the concentration field of gas-phase turbulent jets*
J. Fluid Mech. 218, 109*
1990. `
..21.2,44.3: conservation of momentum, etc., can be worse than for unconfined jets*
HITCHMAN, G.J.; ET AL*
Turbulent plane jet with and without confining end walls*
AIAA J. 28, 1699*
1990. `
..10.0,21.1: normalized stresses higher than in jet, and intermittency spreads closer to center line, implying larger length scales*
CHANDRASEKHARA, M.S.; RAMAPRIAN, B.R.*
Intermittency and length scale distributions in a plane turbulent plume*
J. Fluids Engg. 112, 367*
1990. `
..21.1, 17.1: higher entrainment for given mass flow rate*
BREMHORST, K.; HOLLIS, P.G.*
Velocity field of an axisymmetric pulsed, subsonic air jet*
AIAA J. 28, 2043*
1990. `
..21.2,24.1:  untuned means that jet column frequency is unrelated to shear-layer instability frequency*
THOMAS, F.O.; PRAKASH, K.M.K.*
An experimental investigation of the natural transition of an untuned planar jet*
Phys. Fluids A3, 90*
1991. `
..21.2,18.2:  unprecedented density ratio 0 . 14 to 5 . 11 - Rayleigh scattering.  See p. 135*
PITTS, W.M.*
Effects of global density ratio on the centerline mixing behavior of axisymmetric turbulent jets*
Expts. in Fluids 11, 125*
1991. `
..21.2,04.0:  See p. 125 - virtual origin effects.  Intermittency on centerline tends to 0 . 77*
PITTS, W.M.*
Reynolds number effects on the mixing behavior of axisymmetric turbulent jets*
Expts. in Fluids 11, 135*
1991. `
..11.6,21.2:  fluorescein in water with Sc=2075 - essentially all molecular mixing occurs in thin sheet-like layers*
DAHM, W.J.A.; SOUTHERLAND, K.B.; BUCH, K.A.*
Direct, high resolution, four-dimensional measurements of the fine scale structure of Sc >> 1 molecular mixing in turbulent flows*
Phys. Fluids A3, 1115 (1990 IUTAM Sympo. on Fluid Mech. of Stirring and Mixing)*
1991. `
..11.6,21.2:  better mixing at high Re for given Sc*
MILLER, P.L.; DIMOTAKIS, P.E.*
Reynolds number dependence of scalar fluctuations in a high Schmidt number turbulent jet*
Phys. Fluids A3, 1156*
1991. `
..21.1,02.1:  all 2D - related to Crow.  Stirring not mixing*
STERN, M.E.*
Entrainment of an eddy at the edge of a jet*
J. Fluid Mech. 228, 343*
1991. `
..21.2,24.1:  in the mixing layer of a circular nozzle*
MANKBADI, R.R.*
Multifrequency excited jets*
Phys. Fluids A 3, 595*
1991. `
..11.6,21.1:  helium/air, about 70 percent air, into air.  Joint normal not a good approx. for vel. and rho*
SO, R.M.C.; ZHU, J.Y.; OTUGEN, M.V.; HWANG, B.C.*
Behavior of probability density functions in a binary gas jet*
Expts. in Fluids 11, 227*
1991. `
..21.2,24.1:  PLIF, Re = 3000*
YODA, M.; HESSELINK, L.; MUNGAL, M.G.*
The temporal evolution of large-scale structures in the turbulent jet*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 6-1*
1991. `
..24.1,21.2:  just so - loudspeakers*
RAMAN, G.; RICE, E.J.; RESHOTKO, E.*
Control of an axisymmetric turbulent jet by multi-modal excitation*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 6-2*
1991. `
..24.1,21.0:  direct simulation of pairing of vortex rings - involving hairpin/horseshoe vortex loops*
MELANDER, M.V.; HUSSAIN, F.; BASU, A.*
Breakdown of a circular jet into turbulence*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 15-5*
1991. `
..62.0,21.0:  related to Bradbury*
ZAMAN, K.B.M.Q.; SAMIMY, M.; REEDER, M.F.*
Effect of tabs on the evolution of an axisymmetric jet*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, paper no. 25-5*
1991. `
..19.2,12.1,21.3:  Taylor's hypothesis not good for large strain rates*
RAHAI, H.R.; LaRUE, J.C.*
A comparison of temporal and spatial temperature derivatives in a strained turbulent flow*
Presented at 8th Symposium on Turbulent Shear Flows, Munich, poster no. I-16*
1991. `
..21.3,32.1:  two-point space-time corr. meas. using double Bragg cell*
CENEDESE, A.; ROMANO, G.P.; DiFELICE, F.*
Experimental testing of Taylor's hypothesis by L.D.A. in highly turbulent flow*
Expts. in Fluids 11, 351*
1991. `
..21.1:  variation depends on angle (mom.) of entrainment streamlines, i.e. on far-field b.c.s*
KOTSOVINOS, N.E.; ANGELIDIS, P.B.*
The momentum flux in turbulent submerged jets*
J. Fluid Mech. 229, 453*
1991. `
..54.0,21.2,47.1:  i.e. two annular jets.  All six Reynolds stresses but flow dominated by vortices shed by nozzle lips*
FREY, M.O.; GESSNER, F.B.*
Experimental investigation of coannular jet flow with swirl along a centerbody*
AIAA J. 29, 2132*
1991. `
..14.0,21.1:  k, eps., gamma model where eddy vis. depends on gamma gradient - full paper by Cho and Chung JFM*
KIM, S.K.; CHUNG, M.K.; CHO, J.R.*
Analysis of the effect of initial conditions on the initial development of a turbulent jet*
Presented at 5th Sympo. on Num. and Phys. Aspects of Aerodynamic Flows, Long Beach*
1992. `
..21.1: multi-nozzle rocket*
MORRISEY, D.C.*
Historical perspective - Viking Mars Lander propulsion*
J. Prop. Power 8, 320*
1992. `
..21.1,44.2: ramjet centerbody as projectile in barrel filled with premixed fuel*
BOGDANOFF, D.W.*
Ram accelerator direct space launch system - new concepts*
J. Prop. Power 8, 481*
1992. `
..09.2,21.2: just so*
VAN DUIN, C.A.; JANSSEN, P.A.E.M.*
An analytic model of the generation of surface gravity waves by turbulent air flow*
J. Fluid Mech. 236, 197*
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. `
..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. `
..21.3,20.0: generally larger than mean vel.*
ZHOU, Y.; ANTONIA, R.A.*
Convection velocity measurements in a cylinder wake*
Expts. in Fluids 13, 63*
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. `
..21.3,18.1: isotropic - Taylor OK for vorticity, not dilatation*
LEE, S.; LELE, S.K.; MOIN, P.*
Simulation of spatially evolving turbulence and the applicability of Taylor's hypothesis in compressible flow*
Phys. Fluids A4, 1521*
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. `
..21.0,42.3: published version.  Tests triple-product models based on triple transport equation.  See p. 225*
PANCHAPAKESAN, N.R.; LUMLEY, J.L.*
Turbulence measurements in axisymmetric jets of air and helium.  Part 1.  Air jet.*
J. Fluid Mech. 246, 197*
1993. `
..21.0,42.3: turb. Sc about 0.7, mild buoyancy effect.  Triple-product model tests.  See p. 197*
PANCHAPAKESAN, N.R.; LUMLEY, J.L.*
Turbulence measurements in axisymmetric jets of air and helium.  Part 2.  Helium jet*
J. Fluid Mech. 246, 225*
1993. `
..11.2, 21.3: spatial correlations in all 3 directions. T convection velocity much closer to mean vel. than in zero p.g. Was AIAA-92-0550*
BAGHERI, N.; WHITE, B.R.*
Experimental measurements of large-scale temperature fluctuation structures in a heated incompressible turbulent boundary layer*
Int. J. Heat Mass Transf. 36, 907*
1993. `
..21.2,62.0,54.0: "lift" matters - trailing rather than horseshoe vortices*
SAMIMY, M.; ZAMAN, K.B.M.Q.; REEDER, M.F.*
Effects of tabs on the flow and noise field of an axisymmetric jet*
AIAA J. 31, 609*
1993. `
..62.0,21.2: synoptic - 90 or 160 deg bends in pipe flow, five dia. from jet exit.  Hot wire results*
VRADIS, G.C.; ET AL.*
Round incompressible jets with asymmetric initial velocity distributions*
AIAA J. 31, 814*
1993. `
..21.2,32.1: 3-component meas. in jet and flame up to all 3rd order moments*
FRUCHTEL, G.; ET AL.*
LDA measurements of higher statistical moments for assessment of a Reynolds-stress model*
Engg Turbulence Modelling and Expts 2, (W. Rodi and F. Martelli, Eds.) Elsevier, p. 847*
1993. `
..21.2: different virtual origins for centerline decay and spreading rate - careful experiments at NIST*
RICHARDS, C.D.; PITTS, W.M.*
Global density effects on the self-preservation behaviour of turbulent free jets*
J. Fluid Mech. 254, 417*
1993. `
..21.0: x/D approx 60 - average over 10,000 vectors at each data point*
NINOMIYA, N.; KASAGI, N.*
Measurement of the Reynolds stress budgets in an axisymmetric free jet with the aid of 3-D particle tracking velocimetry*
Presented at 9th Sympo. on Turbulent Shear Flows, Kyoto, paper 6-1*
1993. `
..21.1,23.0: time-dependent. Possible relevance to pressure fluctuations*
MANNO, V.P.; REISTMA, S.H.; TUREAUD, T.F.*
Developing numerical techniques for solving low Mach number fluid-acoustic problems*
AIAA J. 31, 1984*
1993. `
..21.2,42.3: LDA and thermocouple up to triple products. Discusses refraction effect on LDA*
CRESSWELL, R.W.; SZCZEPURA, R.T.*
Experimental investigation into a turbulent jet with negative buoyancy*
Phys. Fluids A5, 2865*
1993. `
..21.1,31.1: Re=100,000. Care taken to avoid recirculation - large enclosure. Flying hot-wire meas. - stationary wires give large errors*
HUSSEIN, H.J.; CAPP, S.P.; GEORGE, W.K.*
Velocity measurements in a high-Reynolds-number, momentum-conserving, axisymmetric, turbulent jet*
J. Fluid Mech. 258, 31*
1994. `
..24.1,21.1,18.1: including "third boundary condition" as required for self-similarity*
KENNEDY, C.A.; GATSKI, T.B.*
Self-similar supersonic variable-density shear layers in binary systems*
Phys. Fluids 6, 662*
1994. `
..21.2,54.0: tabs produce vortex pairs in opposite sense to horseshoe, thrust loss 1-1.5 percent per tab*
ZAMAN, K.B.M.Q.; REEDER, M.F.; SAMIMY, M.*
Control of an axisymmetric jet using vortex generators*
Phys. Fluids 6, 778*
1994. `
..21.3,11.3: time and space derivatives of temperature*
MI, J.; ANTONIA, R.A.*
Corrections to Taylor's hypothesis in a turbulent circular jet*
Phys. Fluids 6, 1548*
1994. `
..21.2,19.2: flying hot wire for mean-square derivatives*
HUSSEIN, H.J.*
Evidence of local axisymmetry in the small scales of a turbulent planar jet*
Phys. Fluids 6, 2058*
1994. `
..18.1,21.1: LRR model fairly good*
RUFFIN, E.; ET AL.*
Investigation of characteristic scales in variable density turbulent jets using a second-order model*
Phys. Fluids 6, 2785*
1994. `
..21.2,30.3: water-driven piston*
PAPANICOLAOU, P.N.*
A piston driven jet for the study of the zone of flow establishment*
Expts. in Fluids 17, 287*
1994. `
..25.6,21.2: filtering of PDV measurements at high Re. Pure eddy vis. poor, dynamic model better*
LIU, S.; MENEVEAU, C.; KATZ, J.*
On the properties of similiarity subgrid-scale models as deduced from measurements in a turbulent jet*
J. Fluid Mech. 275, 83*
1994. `
..11.1,21.1: complexity of contours of positive-definite quantities increases with decreasing level*
LIENAU, J.J; KOLLMANN, W.; CHEN, J.H.*
Structural properties of turbulent round jets*
AIAA 94-0406*
1994. `
..24.1,21.2: two excitation frequencies one octave apart-energy for subharmoic comes directly from mean flow*
PASCHEREIT, C.O.; WYGNANSKI, I.; FIEDLER, H.E.*
Experimental investigation of subharmonic resonance in an axisymmetric jet*
J. Fluid Mech. 283, 365*
1995. `
..44.1,21.0,05.5: water-into-air jet - voids, but not surface tension, discussed*
WOLF, D.H.; INCROPERA, F.P.; VISKANTA, R.*
Measurement of the turbulent flow field in a free-surface jet of water*
Expts in Fluids 18, 397*
1995. `
..21.2,54.0: growth rates correlate with "Richardson number"*
CUTLER, A.D.; LEVEY, B.S.; KRAUS, D.K.*
Near-field flow of supersonic swirling jets*
AIAA J. 33, 876*
1995. `
..21.1,11.2: heated rings in self-pres. region - they were surprised by rapid mixing/stirring*
TONG, C.; WARHAFT, Z.*
Passive scalar dispersion and mixing in a turbulent jet*
J. Fluid Mech. 292, 1*
1995. `
..02.1,21.2: Phillips results and other interface properties little changed*
GHARBI, A. AMIELH, M.; ANSELMET, F.*
Experimental investigation of turbulence properties in the interface region of variable density jets*
Phys. Fluids 7, 2444*
1995. `
..21.3,19.2,11.2: correlation 0.74 for Sc >> 1 in jet*
SOUTHERLAND, K.B.; DAHM, W.J.A.*
Experimental assessment of Taylor's hypothesis and its applicability to dissipation estimates in turbulent flows*
Presented at 10th Sympo. on Turbulent Shear Flows, Penn. State, paper 1-13*
1995. `
..17.1,21.0: linear or quadratic acceleration -reduced spreading rate*
ZHANG, Q.; JOHARI, H.*
Experiments on accelerating turbulent jets*
Presented at 10th Sympo. on Turbulent Shear Flows, Penn. State, paper 9-19*
1995. `
..21.2,13.0: length scale ratio constant, as assumed in modeling*
FRUCHTEL, G,; HASSEL, E.P.; JANICKA, J.*
Spatial velocity correlations in a turbulent jet*
Presented at 10th Sympo. on Turbulent Shear Flows, Penn. State, paper 12-1*
1995. `
..11.2,21.0: fluorescein in water with laser to excite. Reynolds number up to 700000 - no 5/3 law*
MILLER, L.; DIMOTAKIS, E.*
Measurements of scalar power spectra in high Schmidt number turbulent jets*
J. Fluid Mech. 308, 129*
1996. `
..24.1,21.1,31.1: cross wires, with dv/dt replacing dv/dx*
RAJAGOPALAN, S.; KO, N.W.M.*
Velocity and spanwise vorticity measurements in an excited mixing layer of a plane jet*
Expts in Fluids 20, 346*
1996. `
....17.1,21.2: large increase in entrainment*
BOREE, J.; ATASSI, N.; CHARNAY, G.*
Phase averaged velocity field in an axisymmetric jet subject to a sudden velocity decrease*
Expts. in Fluids 21, 447*
1996. `
..11.6,19.2,21.2: Sc = 2000. Scalar dissipation in sheet-like diffusion layers*
BUCH. K.A.; DAHM, W.J.A.*
Experimental study of the fine-scale structure of conserved scalar mixing in turbulent shear flows.  Part 1. Sc >> 1*
J. Fluid Mech. 317, 21*
1996. `
..11.6,21.2: LIF around the mixing-transition range of Re*
CATRAKIS, H.J.; DIMOTAKIS, P.E.*
Mixing in turbulent jets - scalar measures and isosurface geometry*
J. Fluid Mech. 317, 369*
1996. `
..18.2,21.2: density ratio 0.14 to 1.5. Half - width little altered. LDV meas. including TKE budget*
DJERIDANE, T; ET AL.*
Velocity turbulenc properties in the near-field region of axisymmetric variable density jets*
Phys. Fluids 8, 1614*
1996. `
..25.6,21.1: dynamic SGS model with bound for coefficient based on non-negativity of total dissipation. Re up to 5 x 10^5*
OLSSON, M.; FUCHS, L.*
Large eddy simulation of the proximal region of a spatially developing circular jet*
Phys. Fluids 8, 2125*
1996. `
..17.1,21.2: i.e. time-dependent exit velocity. Flow viz. and simple theory*
ZHANG, Q.; JOHARI, H.*
Effects of acceleration on turbulent jets*
Phys. Fluids 8, 2185*
1996. `
..21.2,53.0: one-compt. LDV in round jet*
OTUGEN, M.V.; GIRLEA, F.; STORZA, P.M.*
The turbulent incompressible jet in a curved coflow*
J. Fluids Engg. 118, 300*
1996. `
..09.2,21.2: particles smaller than Kolmogorov length scale. LDV meas.*
SATO, Y.; HISHIDA, K.; MEEDA, M.*
Effect of dispersed phase on modification of turbulent flow in a wall jet*
J. Fluids Engg. 118, 307*
1996. `
..11.6,21.2: dye in water, Sc=3800, Re=6400*
NAKAMURA, I.; ET AL.*
Measurements of velocity-scalar joint statistics in an axisymmetric turbulent jet*
Presented at 1996 Mtg of Japan Society of Fluid Mech., preprint volume p. 79*
1996. `
..32.2,21.2: Tokyo Inst. Tech. work*
KOBAYASHI, K.P.; ET AL.*
Measurement of the evolving large eddies in axisymmetric jets from traversing camera by using cross-correlation technique*
1st Pacific Sympo. on Flow Visualization and Image Processing*
1997. `
..24.1,18.1,21.2: time-dependent, M_c up to 0.99*
FREUND, J.B.; LELE, S.K.; MOIN, P.*
Direct simulation of a supersonic round turbulent shear layer*
AIAA 97-0760*
1997. `
..21.2,54.0: up to 60 percent increase in mixing rate (see NPL Aero 1116)*
NAUGHTON, J.W.; CATTAFESTA, L.N. III; SETTLES, G.S.*
An experimental study of compressible turbulent mixing enhancement in swirling jets*
J. Fluid Mech. 330, 271*
1997. `
..19.2,21.2: high-k intermittency. Circular jet at microscale Re up to 300*
CAMUSSI, R.; BARBAGALLO, D.*
Experimental analysis of transverse intermittency in a turbulent jet flow*
Expts. in Fluids 22, 268*
1997. `
..17.1,21.2; Re up to 20000 - starting vortex ring detaches*
JOHARI, H.; ET AL.*
Impulsively started turbulent jets*
AIAA J. 35, 657*
1997. `
..14.0,21.2: several adverse comments on Thies and Tam 1996*
BIRCH, S.F.*
Comment on "Computation of turbulent axisymmetric and nonaxisymmetric jet flows using the k, eps. model"*
AIAA J. 35, 760*
1997. `
..1.1,21.2: effect of vortex rings at low Re - enhanced by acoustic excitation*
SEOL, W.S.; GOLDSTEIN, R.J.*
Energy separation in a jet flow*
J. Fluids Engg 119, 74*
1997. `
..18.1,24.1,21.3: notes the spread in convection velocity but attributes it to structure interaction - tripling not doubling*
DUPONT, P.; MUSCAT, P.; DUSSAUGE, J.P.*
Localization and analysis of large scale structures by a wavelet transform technique in a supersonic turbulent mixing layer*
Presented at 11th Sympo. on Turbulent Shear Flows, Grenoble, paper 29-8*
1997. `
..21.3,11.2: conserved scalar in x,y,z,t. Sc = 2075. Correlation of streamwise gradient and T's H. Estimate is 0.74 in region of max. intensity in jet*
DAHM, W.J.A.; SOUTHERLAND, K.B.*
Experimental assessment of Taylor's hypothesis and its applicability to dissipation estimates in turbulent flows*
Phys. Fluids 9, 2101*
1997. `
..21.2: Reynolds numbers 7000 - 100,000. Simple checks of initial conditions*
MALMSTROM, T.G.; ET AL.*
Centerline velocity decay measurements in low-velocity axisymmetric jets*
J. Fluid Mech. 346, 363*
1997. `
..21.2,17.1,14.0: k, eps. poor because of negative production*
BREMHORST, K.; GEHRKE, P.; HE, S.*
Measured Reynolds stress distributions and energy budgets of fully pulsed round free jets and comparisons with k, eps. model predictions*
Presented at 11th Sympo. on Turbulent Shear Flows, Grenoble, Paper 22-1*
1997. `
..21.2,25.6: Lesieur structure-function SGS model - inclined vortex rings and excited blooming at Re = 20000*
URBIN, G.; BRUN, C.; METAIS, O.*
Large eddy simulations of three-dimensional spatially evolving round jets*
Presented at 11th Sympo. on Turbulent Shear Flows, Grenoble, Paper 25-23*
1997. `
..21.2,62.0:  outer velocity >> inner, with recirculation for factor > 8. Re=10000 to 100000 - transitional*
REHAB, H.; VILLERMAUX, E.; HOPFINGER, E.J.*
Flow regimes of large-velocity-ratio coaxial jets*
J. Fluid Mech. 345, 357*
1997. `
..21.2,24.1:  significant Re effects between 5500 and 16000 at x/d up to 30.  DPIV meas. up to triple (scattered)*
WEISGRABER, T.H.; LIEPMANN, D.*
Turbulent structure during transition to self-similarity in a round jet*
Expts. in Fluids 24, 210*
1998. `
..21.2: DNS - suggests nonuniversal similarity, but Re only 2400 and x<45D*
BOERSMA, B.J.; BRETHOUWER, G.; NIEUWSTADT, F.T.M.*
A numerical investigation on the effect of the inflow conditions on the self-similar region of a round jet*
Phys. Fluids 10, 899*
1998. `
..54.0,21.2:  Re = 2800.  Complex clam-like structure*
WEBSTER, D.R.; LONGMIRE, E.K.*
Vortex rings from cylinders with inclined exits*
Phys. Fluids 10, 400*
1998. `
..21.3:  space-time correlations of u component only - definition of U_c not clear, but different for ejections, sweeps etc.*
KROGSTAD, P.-A.; KASPERSEN, J.H.; RIMESTAD, S.*
Convective velocities in a turbulent boundary layer*
Phys. Fluids 10, 949*
1998. `
..11.6,21.2:  significant with Sc ratios of 4 and 18 (available Sc range 1200 to 77000)*
SAYLOR, J.R.; SREENIVASAN, K.R.*
Differential diffusion in low Reynolds number water jets*
Phys. Fluids 10, 1135*
1998. `
..21.2,18.2:  mainly an issue of initial conditions.  Big virtual-origin effects*
ZAMAN, K.B.M.Q.*
Asymptotic spreading rate of initially compressible jets - experiments and analysis*
Phys. Fluids 10, 2652*
1998. `
..21.2: scales virtual-origin shift (including Reynolds-number effects)*
PAPADOPOULOS, G.; PITTS, W.M.*
A generic centerline velocity decay curve for initially turbulent axisymmetric jets*
J. Fluids Engg 121, 80*
1999. `
..22.1,21.1:  Re = 5000, 0.4 < centerline M < 1.2*
MITCHELL, B.E.; LELE, S.K.; MOIN, P.*
Direct computation of the sound generated by vortex pairing in an axisymmetric jet*
J. Fluid Mech. 383, 113*
1999. `
..21.2:  "substantial increases in mixing".  HWA and crossed-vane vorticity probe*

BOHL, D.G.; FOSS, J.F.*
Near exit plane effects caused by primary and primary-plus-secondary tabs*
AIAA J. 37, 192*
1999. `
..32.2,11.2,21.2:  particle tracking - more vectors than PIV*
WEBSTER, D.R.; ROBERTS, P.J.W.; RA'AD, L.*
Simultaneous DPTV/PLIF measurements of a turbulent jet*
To be presented at 3rd International Workshop on Particle Image Velocimetry, Santa Barbara, CA*
1999. `
..32.0,21.3:  cross-correlation between image pair*
SMITH, K.M.; DUTTON, J.C.*
A procedure for turbulent structure convection velocity measurements using time-correlated images*
Expts. in Fluids 27, 244*
1999. `
..48.0,21.3:  longitudinal component and longitudinal separation only*
ROMANO, G.P.; ANTONIA, R.A.; ZHOU, T.*
Evaluation of LDA temporal and spatial velocity structure functions in a low Reynolds number turbulent channel flow*
Expts. in Fluids 27, 368*
1999. `
..25.6,21.2:  Smago., dynamic S. and dynamic mixed models.  Last two about equal*
RIBAULT, C.L.; SARKAR, S.; STANLEY, S.A.*
Large eddy simulation of a plane jet*
Phys. Fluids 11, 3069*
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. `
..21.2:  DNS to investigate initial conditions, numerical accuracy etc. - concludes that jet is too sensitive to be universal*
TAKEUCHI, S.; MIYAKE, Y.; KAJISHIMA, T.*
Decay of a round jet*
Turbulence and Shear Flow Phenomena - 1 (S. Banerjee and J.K. Eaton, Eds.), Begell House, p. 1181*
1999. `
..21.3,18.2:  specifically, decay of space-time correlations.  Convection velocity not explicitly deduced*
UNALMIS, O.H.; DOLLING, D.S.*
Decay of fluctuating wall-pressure field of Mach 5 turbulent boundary layer*
AIAA J. 37, 1088*
1999. `
..17.1,21.2,31.1:  careful hot-wire calibration, but intensities are very high.  Pulses still identifiable at x/d = 70 but fd/U only 0.0035*
BREMHORST, K.; GEHRKE, P.J.*
Measured Reynolds stress distributions and energy budgets of a fully pulsed round air jet*
Expts in Fluids 28, 519*
2000. `
..21.2,01.1,31.1:  two spanwise-separated rakes of 8 x-wires each*
GORDEYEV, S.V.; THOMAS, F.O.*
Coherent structure in the turbulent planar jet.  Part I.  Extraction of proper orthogonal decomposition eigenmodes and their self-similarity*
J. Fluid Mech. 414, 145*
2000. `
..25.6,21.2:  dynamic Smago*
WEBB, A.T.; MANSOUR, N.N.*
Towards LES models of jets and plumes*
Annual Research Briefs - 2000, Ames/Stanford Center for Turbulence Research, 229*
2000. `
..21.3:  calculations of "Taylor" and true accelerations based on assumed structure functions.  Hypothesis valid for microscale Re > 1000, "questionable" for Re < 100*
PINSKY, M.; KHAIN, A.; TSINOBER, A.*
Accelerations in isotropic and homogeneous turbulence and Taylor's hypothesis*
Phys. Fluids 12, 3195*
2000. `
..22.1,21.2:  good agreement with simulations*
COLONIUS, T.; FREUND, J.B.*
Application of Lighthill's equation to a Mach 1.92 turbulent jet*
AIAA J. 38, 368*
2000. `
..21.3:  convection vel. in M = 1.5 He-air jet supersonic w.r.t. ambient air - Mach waves seen*
MURAKAMI, E.; PAPAMOSCHOU, D.*
Eddy convection in coaxial supersonic jets*
AIAA J. 38, 628*
2000. `
..21.2:  rectangular nozzles with one or two cutouts on one side*
KIM, J.-H.; SAMIMY, M.*
On mixing enhancement via nozzle trailing-edge modifications in high-speed jets*
AIAA J. 38, 935*
2000. `
..21.2,17.1:  DNS with pulsed injection simulated by body forces*
FREUND, J.B.; MOIN, P.*
Jet mixing enhancement by high-amplitude fluidic actuation*
AIAA J. 38, 1863*
2000. `
..21.2,48.0:  triangle to hex, in order of decreasing increment in jet dia. at x/D = 10*
SRINIVASAN, K.; RATHAKRISHNAN, E.*
Studies on polygonal slot jets*
AIAA J. 38, 1985*
2000. `
..21.1,25.6:  Blake's hydrofoil.  Dynamic SGS model*
WANG, M.; MOIN, P.*
Computation of trailing-edge flow and noise using large-eddy simulation*
AIAA J. 38, 2201*
2000. `
..21.2,32.2:  accurate self-similarity in far-field.  Re = 3000*
WEBSTER, D.R.; ROBERTS, P.J.W.; RA'AD, L.*
Simultaneous DPTV/PLIF measurements of a turbulent jet*
Expts. in Fluids 30, 65*
2001. `
..19.2,21.2:  significant - explains disagreement between previous results*
ROMANO, G.P.; ANTONIA, R.A.*
Longitudinal and transverse structure functions in a turbulent round jet -  effect of initial conditions and Reynolds number*
J. Fluid Mech. 436, 231*
2001. `
..21.2:  one "top hat" exit profile, one fully-developed pipe flow.  Normalized to same momentum flux and exit temperature (should be heat flux) but ratio of r.m.s. T fluc. to mean T difference is meaningful and depends on exit condition to x/d = 70 at least*
MI, J.; NOBES, D.S.; NATHAN, G.J.*
Influence of jet exit conditions on the passive scalar field of an axisymmetric free jet*
J. Fluid Mech. 432, 91*
2001. `
..19.2,21.2:  12 million HWA velocity samples in a jet.  Longitudinal velocity increment is Markovian and leads to Fokker-Planck equation for its p.d.f.*
RENNER, C.; PEINKE, J.; FRIEDRICH, R.*
Experimental indications for Markov properties of small-scale turbulence*
J. Fluid Mech. 433, 383*
2001. `
..62.0,21.2:  LES but with thin laminar exit BLs, Re up to 220000.  Mainly square but AR up to 4 entrainment up to 1.4 time circular jet with some hydraulic dia.*
GRINSTEIN, F.F.*
Vortex dynamics and entrainment in rectangular free jets*
J. Fluid Mech. 437, 69*
2001. `
..62.0,21.2:  "considerable mixing enhancement"
BITTING, J.W.; ET AL.*
Visualization and two-color DPIV measurements of flows in circular and square coaxial nozzles*
Expts. in Fluids 31, 1*
2001. `
..32.2,21.2:  just so - tomography provides the large data sets needed for POD*
PELLICCIA-KRAFT, B.J.; WATT, D.W.*
Visualization of coherent structure in scalar fields of unsteady jet flows with interferometric tomography and proper orthogonal decomposition*
Expts. in Fluids 30, 633*
2001. `
..22.1,21.2:  DNS and accurate computation of Lighthill T_ij source term*
FREUND, J.B.*
Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9*
J. Fluid Mech. 438, 277*
2001. `
..19.2,21.2:  high k.  Camussi jet data (e.g. EF 22, 268, 1997)*
NIKORA, V.; GORING, D.; CAMUSSI, R.*
Intermittency and interrelationships between turbulence scaling exponents - phase-randomization tests*
Phys. Fluids 13, 1404*
2001. `
..24.1,21.2:  top-hat and fully-developed pipe profiles.  Spectra collapse for x>30d*
ANTONIA, R.A.; ZHAO, Q.*
Effect of initial conditions on a circular jet*
Expts. in Fluids 31, 319*
2001. `
..42.3,21.2:  flow viz. shows fairly sudden fall in growth rate at x/l_N = 2.9, where l_N = M^{1/4}/N^{1/2} and M is thrust/density*
WEBSTER, D.R.; LIU, Y.*
Velocity measurements of turbulence collapse in a linearly stratified jet*
Expts. in Fluids 31, 394*
2001. `
..05.0,21.3:  convection vel. in viscous sublayer 15u_tau for BL Re 2900-4100, slightly less in duct. Part 1 (not so labeled) is 29, 448*
KHOO, B.C.; CHEW, Y.T.; TEO, C.J.*
Near-wall hot-wire measurements.  Part II - Turbulence time scale, convective velocity and spectra in the viscous sublayer*
Expts. in Fluids 31, 494*
2001. `
..02.1, 21.2: combined PIV/LIF: Burgersdag poster only*
WESTERWEEL, J.; ET AL.*
The turbulent/non-turbulent interface at the outer boundary of a jet*
Burgers Centrum newsletter 2002.1, TU Delft*
2002. `