..13.0: need a nonlinear "slow" part*
LASHER, W.C.; TAULBEE, D.B.*
Calculation of turbulent backstep flow - Commentary on modelling of the pressure-strain correlation*
Engineering Turbulence Modeling and Experiments*
1990. `
..16.2,53.0:final writeup*
BASKARAN, V.; PONTIKIS, Y.G.; BRADSHAW, P.*
Experimental investigation of three-dimensional turbulent boundary layers on "infinite" curved swept wings*
J. Fluid Mech. 211, 95*
1990. `
..17.1,14.0:2D infinite plate and "Ekman"*
JUSTESEN, P.; SPALART, P.R.*
Two-equation turbulence modeling of oscillatory boundary layers*
AIAA-90-0496*
1990. `
..12.2,22.2: general review and mentions of new large facilities suggested at Grenoble workshop*
FRISCH, U.; ORSZAG, S.A.*
Turbulence - challenges for theory and experiment*
Physics Today, vol. 43, no. 1, p. 24*
1990. `
..28.3:son et lumiere - series of articles*
TAZELAAR, J.M.*
Multimedia*
BYTE vol. 15, no. 2, p. 200*
1990. `
..28.3: possibility of 3D storage, etc*
VOGELGESANG, P.*
Drowning in data*
BYTE vol. 15, no. 2, p. 251*
1990. `
..28.3: useful intro.*
POUNTAIN, R.*
Object-oriented programming*
BYTE vol. 15, no. 2, p. 257*
1990. `
..50.0,11.3: intensities up to 19 percent, and up to 26 percent increase in heat transfer*
AMES, F.E.; MOFFAT, R.J.*
Effects of simulated combustor turbulence on boundary layer heat transfer*
To be presented at AIAA Seattle meeting, June*
1990. `
..12.2: models of simultaneous cascade of more than one variable*
MENEVEAU, C.; SREENIVASAN, K.R.; KAILASNATH, P.; FAN, M.S.*
Joint multifractal measures - theory and applications to turbulence*
Phys. Rev. A 41, 894*
1990. `
..50.0,11.3: based on max u fluctuation, which is said to equal free stream if latter high enough*
MACIEJEWSKI, P.K.; MOFFAT, R.J.*
A correlation for boundary layer heat transfer accounting for free stream turbulence*
Submitted to 9th Int. Heat Transfer Conf., Jerusalem*
1990. `
..19.3: shot-noise model*
VEERAVALLI, S.V.; VEERAVALLI, V.V.*
Higher-order spectra of turbulent velocity fluctuations*
Submitted to Phys. Fluids A (unpublished?)*
1990. `
..13.0: good job on proper wall behavior -- but a damping factor depends on bulk Re*
SHIH, T.H.*
Second order modeling of low Reynolds number turbulence near walls*
Submitted to Phys. Fluids*
1990. `
..14.0,25.5: Huntsville work -- FLUENT with k, eps.*
MAJUMDAR, A.K.; ET AL.*
Effect of idealized asymmetric inhibitor stubs on circumferential flow in the space shuttle SRM*
J. Prop. Power 6, 5*
1990. `
..09.5: (no suitable index category) -- negative masses do not violate Newton's laws.  Not the same as antimatter*
FORWARD, R.L.*
Negative matter propulsion*
J. Prop. Power 6, 28*
1990. `
..59.0,54.0: Wright-Patt. work -- low speed, LDV and hot film*
SAMIMY, M.; ET AL.*
Nonaxisymmetric instabilities in a dump combustor with a swirling inlet flow*
J. Prop. Power 6, 78*
1990. `
..22.2: name due to Sommerfeld*
ROTT, N.*
Note on the history of the Reynolds number*
Ann. Rev. Fluid Mech. 22, 1*
1990. `
..59.2: including stability*
DRELA, M.*
Aerodynamics of human-powered flight*
Ann. Rev. Fluid Mech. 22, 93*
1990. `
..12.2,11.1: more specialized than book*
OTTINO, J.M.*
Mixing, chaotic advection, and turbulence*
Ann. Rev. Fluid Mech. 22, 207*
1990. `
..25.3: general review*
HESS, J.L.*
Panel methods in computational fluid dynamics*
Ann. Rev. Fluid Mech. 22, 255*
1990. `
..12.2: plasma as distinct from MHD*
SIMILON, P.L.; SUDAN, R.N.*
Plasma turbulence*
Ann. Rev. Fluid Mech. 22, 317*
1990. `
..47.2,59.2: also see Joubert and Larsson book*
LARSSON, L.*
Scientific methods in yacht design*
Ann. Rev. Fluid Mech. 22, 349*
1990. `
..30.3,24.4,18.2: mainly hypersonics*
BECKWITH, I.E.; MILLER, C.G.*
Aerothermodynamics and transition in high-speed wind tunnels at NASA Langley*
Ann. Rev. Fluid Mech. 22, 419*
1990. `
..24.2: just so -- 60 pages on absolute vs. convective instability*
HUERRE, P.; MONKEWITZ, P.A.*
Local and global instabilities in spatially developing flows*
Ann. Rev. Fluid Mech. 22, 473*
1990. `
..59.0: mainly discussion of absolute instability*
OERTEL, H.*
Wakes behind blunt bodies*
Ann. Rev. Fluid Mech. 22, 539*
1990. `
..16.2,45.0: concentrating on separation over nose*
JONES, G.S.*
The hemisphere-cylinder at an angle of attack*
AIAA-90-0050, Reno conference*
1990. `
..54.0,59.2: McDonnell work -- discussion of breakdown*
HAWK, J.; BARNETT, R.; O'NEIL, P.*
Investigation of high angle of attack vortical flow over delta wings*
AIAA-90-0101, Reno conference*
1990. `
..14.0: Texas A&M -- extension of Schiestel for k, eps.*
KO, S.H.; RHODE, D.L.*
Derivation and testing of a new multi-scale k, eps. turbulence model*
AIAA-90-0243, Reno conference*
1990. `
..14.0: ASM -- Lewis work*
DEMUREN, A.*
Calculation of turbulence-driven secondary motion in ducts with arbitrary cross-section*
AIAA-90-0245, Reno conference*
1990. `
..60.0: just so -- 152 references*
SETTLES, G.S.*
Swept shock/boundary-layer interactions -- tutorial and update*
AIAA-90-0375, Reno conference*
1990. `
..13.0: pressure-strain model -- fairly arbitrary assumptions*
LIN, A.*
On the mathematical modeling of the Reynolds stress's equations*
AIAA-90-0498, Reno conference*
1990. `
..54.0,59.2: see also 0101. Bursts without recirculation*
KEGELMAN, J.T.; ROOS, F.W.*
The flowfields of bursting vortices over moderately swept delta wings*
AIAA-90-0599, Reno conference*
1990. `
..05.0: latest stage -- including pairs of hairpins*
LIU, N.; SHAMROTH, S.; MCDONALD, H.*
Reciprocal interactions of hairpin-shaped vortices and a boundary layer*
AIAA-90-0017, Reno conference*
1990. `
..14.0: eddy viscosity method -- see AIAA-88-0221 for details of model equation for TKE transfer rate*
KIM, S.*
Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model*
AIAA-90-0047, Reno conference*
1990. `
..49.0: 16, 20, 24 deg. -- thin entry BLs*
ZAMAN, K.; DAHL, M.*
Some observations on transitory stall in conical diffusers*
AIAA-90-0048, Reno conference*
1990. `
..04.0,24.4: small -- but VITA detection frequency depends on Re for Re, theta less than 2700*
WARK, C.E.; HUR, S.W.; NAGUIB, A.M.*
Effects of transition on the Reynolds-stress producing events in a turbulent boundary layer*
AIAA-90-0497, Reno conference*
1990. `
..24.1,18.1: interaction with subharmonic*
RAGAB, S.A.; WU, J.L.*
Instabilities of supersonic shear flows*
AIAA-90-0712, Reno conference*
1990. `
..54.0,59.2,23.0: Ames work -- peaky spectra*
McINERNY, S.A.; MEECHAM, W.C.; SODERMAN, P.T.*
Pressure fluctuations in the tip region of a blunt-tipped airfoil*
AIAA J. 28, 6*
1990. `
..59.2,48.0: chord Re 3 million, no trips on slat, aerofoil or flap*
NAKAYAMA, A.; KREPLIN, H.-P.; MORGAN, H.L.*
Experimental investigation of flowfield about a multielement airfoil*
AIAA J. 28, 14*
1990. `
..17.2: no measurements over aerofoil, Re only 50000*
PARK, S.O.; KIM, J.S.; LEE, B.I.*
Hot-wire measurements of near wakes behind an oscillating airfoil*
AIAA J. 28, 22*
1990. `
..60.0,61.0: review of fins*
LU, F.K.; SETTLES, G.C.; HORSTMAN, C.C.*
Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions*
AIAA J. 28, 91*
1990. `
..19.1,11.1: timescale ratio determined by initial spectrum -- permanence of large eddies*
LEWALLE, J.*
Decay of velocity and temperature fluctuations in grid turbulence*
AIAA J. 28, 106*
1990. `
..14.0,53,0: calcs -- replaces AIAA J. 27, 23, 1989*
DEGANI, D.; SMITS, A.J.*
Effect of short regions of surface curvature on compressible turbulent boundary layers*
AIAA J. 28, 113*
1990. `
..60.0,61.0: fin at M=3*
KIM, K.-S.; SETTLES, G.S.*
Skin friction measurements by laser interferometry in swept shock/boundary-layer interactions*
AIAA J. 28, 133*
1990. `
..29.2: see also AIAA J. 25, 567*
KAZIMIERSKI, Z.; HORODKO, L.*
Total pressure averaging by small-diameter tubes in pulsating flows*
AIAA J. 28, 140*
1990. `
..54.0,59.2: laminar -- bubble-type breakdown with recirculation, starting at x/c = 0 . 6*
THOMAS, J.L.; KRIST, S.T.; ANDERSON, W.K.*
Navier-Stokes computations of vortical flos over low-aspect-ratio wings*
AIAA J. 28, 205*
1990. `
..54.0,59.2: Rensselaer work for parallel vortex -- relevant to helicopter noise*
STRAUS, J.; RENZONI, P.; MAYLE, R.E.*
Airfoil pressure measurements during a blade-vortex interaction and a comparison with theory*
AIAA J. 28, 222*
1990. `
..09.3: 1985 work -- 2 flat-plate LEBUs*
GUEZENNEC, Y.G.; NAGIB, H.M.*
Mechanisms leading to net drag reduction in manipulated turbulent boundary layers*
AIAA J. 28, 245*
1990. `
..59.0: LDV meas. including triple products, starting at x/h = 0 . 2*
GOULD, R.D.; STEVENSON, W.H.; THOMPSON, H.D.*
Investigation of turbulent transport in an axisymmetric sudden expansion*
AIAA J. 28, 276*
1990. `
..24.2: horseshoes*
BIRINGEN, S.*
Numerical simulation of nonlinear structures in channel flow transition*
AIAA J. 28, 365*
1990. `
..25.6: mainly Rogers homo. results*
MOIN, P.*
Similarity of organized structures in turbulent shear flows*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 2*
1990. `
..24.2,25.6: 128^3 simulation of Klebanoff-type peak-valley splitting*
GILBERT, N.; KLEISER, L.*
Near-wall phenomena in transition to turbulence*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 7*
1990. `
..24.2,12.2: attractor and calcs. for 2D disturbances*
JIMENEZ, J.*
Bifurcations and turbulence in plane Poiseuille flow*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 28*
1990. `
..25.6: stochastic estimation and orthogonal decomposition*
MOSER, R.D.*
Statistical analysis of near-wall structures in turbulent channel flow*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 45*
1990. `
..12.2: sane view of not-very-stable attractors for turbulence - refers to eddies as "identifiable structures within the stochastic stew"*
KEEFE, L.R.*
Connecting coherent structures and strange attractors*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 63*
1990. `
..05.0,25.6: slender body calcs., homo. in x, following Hatzi. and Chapman*
HANRATTY, T.J.*
A conceptual model of the viscous wall region*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 81*
1990. `
..41.0: just so*
BRADSHAW, P.*
Effects of extra rates of strain - review*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 106*
1990. `
..50.0: normal plate plus splitter - review of Surrey work*
CASTRO, I.C.*
Free-stream turbulence effects on separated shear layers*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 123*
1990. `
..50.0: especially outer-layer structure*
DYBAN, E.P.; EPIK, E.Y.*
External flow turbulization effect of the wall turbulence structure*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 139*
1990. `
..53.0,05.0: significant effects on log law additive constants*
GIBSON, M.M.*
Effects of surface curvature on the law of the wall*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 157*
1990. `
..50.0,09.4,24.4: the works*
KOZLOV, V.E.; KUZNETSOV, V.R.; MINEEV, B.I.; SEKUNDOV, A.N.*
The influence of free-stream turbulence and surface ribbing on the characteristics of a transitional boundary layer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 172*
1990. `
..60.0,17.1,23.0: no direct effects of shock oscillation on downstream turbulence*
SELIG, M.S.; SMITS, A.J.*
The dynamic behavior of a shock-wave/turbulent boundary layer interaction*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 190*
1990. `
..05.0: just so - part II by  Robinson, Kline and Spalart*
KLINE, S.J.; ROBINSON, S.K.*
Quasi-coherent structures in the turbulent boundary layer - Part I. Status report on a community-wide summary of the data*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 200*
1990. `
..05.0,01.1: just so*
ROBINSON, S.K.; KLINE, S.J.; SPALART, P.R.*
Quasi-coherent structures in the turbulent boundary layer - Part II. Verification and new information from a numerically simulated flat-plate layer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 218*
1990. `
..05.0,01.1: template is artificial hairpin in subcritical lam. BL*
SMITH, C.R.; LU, L.J.*
The use of a template-matching technique to identify hairpin vortex flow structures in turbulent boundary layers*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 248*
1990. `
..05.0: low-speed streaks and streamwise vortices*
BLACKWELDER, R.F.; SWEARINGEN, J.D.*
The role of inflectional velocity profiles in wall bounded flows*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 268*
1990. `
..29.6,46.0,02.1: 18 pairs of photos at short intervals*
UTAMI, T.; BLACKWELDER, R.F.*
Flow visualisation with image processing of three-dimensional features of coherent structures in an open-channel flow*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 289*
1990. `
..05.0: very odd non-monotonic variation of burst frequency with y*
WARK, C.E.; NAGIB, H.M.*
On the character of turbulence-producing events in near-wall turbulence*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 306*
1990. `
..23.0; numerical, computational and transducer resolution*
ECKELMANN, H.*
A review of knowledge on pressure fluctuations*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 328*
1990. `
..23.0,05.0: survey of Gottingen work*
DINKELACKER, A.*
Relations between wall pressure fluctuations and velocity fluctuations in turbulent pipe flow*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 348*
1990. `
..23.0,05.0: pressure as diagnostic*
KOBASHI, Y.; ICHIJO, M.*
Relation between wall pressure and turbulence structure*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 361*
1990. `
..05.0,23.0: VITA - but centering the structures in spanwise position*
JOHANSSON, A.V.; ALFREDSSON, P.H.; KIM, J.*
Velocity and pressure fields associated with near-wall turbulence structures*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 368*
1990. `
..23.0,05.0: k^(-1) and all that*
PANTON, R.L.*
Inner-outer structure of the wall-pressure correlation function*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 381*
1990. `
..05.0,23.0: primarily associated with v - but also large w*
HARITONIDIS, J.H.; GRESKO, L.S.; BREUER, K.S.*
Wall pressure peaks and wakes*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 397*
1990. `
..01.1: fairly detailed review of results*
ADRIAN, R.J.*
Linking correlations and structure - stochastic estimation and conditional averaging*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 420*
1990. `
..12.1,13.0: refers to transport equation for space-time correlations*
DUMAS, R.*
Observations on the boundary layer based on measured correlations with various improvements*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 437*
1990. `
..01.0,05.0: using 1985 unconditional data*
GUEZENNEC, Y.G.; CHOI, W.C.*
Stochastic estimation of coherent structures in turbulent boundary layers*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 453*
1990. `
..01.0: general review*
GEORGE, W.K.*
Insight into the dynamics of coherent structures from a proper orthogonal decomposition*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 469*
1990. `
..04.0,02.1: confined below R, theta = 5000 - more effect on u correlations than v*
ANTONIA, R.A.; BROWNE, L.W.B.; BISSET, D.K.*
Effect of Reynolds number on the organized motion in a turbulent boundary layer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 488*
1990. `
..53.0: Gillis-like rig - large-eddy inclination angle increases in relaxation region*
ALVING, A.E.; SMITS, A.J.*
Correlation measurements and structure angles in a turbulent boundary layer recovering from convex curvature*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 507*
1990. `
..11.2: Summary lecture - see Proc. 8th Int. Conf of Heat and Mass Transf., 1986*
KHABAKHPASHEVA, E.M.*
Structure of turbulence in heat transfer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 544*
1990. ` 
..11.4,05.0,31.2: V-wire and cold wire*
NAGANO, Y.; HISHIDA, M.*
Turbulent heat transfer associated with coherent structures near the wall*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 568*
1990. `
..11.4: transient wall heat flux in water - interesting but inconclusive*
PEREPELITSA, B.V.*
Effect of turbulent flow structure on temperature field formation in near-wall region*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 582*
1990. `
..11.2: review of Tokyo work - e.g. Iritani, Hirata*
KASAGI, N.*
Structural study of near-wall turbulence and its heat transfer mechanism*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 596*
1990. `
..11.2: correlations in yz plane may imply longitudinal vortices*
SLANCIAUSKAS, A.*
Spatial correlations of the temperature fluctuation in boundary layers*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 620*
1990. `
..11.4,03.0,05.0: sharp rise in Pr,t near wall, and decrease in analogy factor in negative p.g.*
KAYS, W.M.; MOFFAT, R.J.*
The near-wall region of the turbulent boundary layer - some results from heat transfer measurements*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 630*
1990. `
..50.0,11.3: factor of five increases in "jet flow"*
MACIEJEWSKI, P.K.; MOFFAT, R.J.*
The effects of high free-stream turbulence on heat transfer in turbulent boundary layer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 640*
1990. `
..05.0,25.6,12.2: suggests bursts produced autonomously by inner layer but triggered by outer layer*
AUBRY, N.; HOLMES, P.; LUMLEY, J.L.; STONE, E.*
Behavior of coherent structures in the wall region by dynamical systems theory*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 672*
1990. `
..24.2: 3D - interaction between mean flow and first harmonic*
BENNEY, D.J.*
Wave interaction and stability problems*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 692*
1990. `
..05.0,24.2: x and z-wise averaged eqns based on Orr Somm. and assuming wall law*
GESHEV, P.I.*
On mathematical formulation of near-wall turbulence problem*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 701*
1990. `
..05.0,12.12: latest version*
PERRY, A.E.; LI, J.D.; HENBEST, S.M.; MARUSIC, I.*
The attached eddy hypothesis in wall turbulence*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 715*
1990. `
..05.0: vortex pairs - for the equations see Andrews and McIntyre JFM 89, 609*
PHILLIPS, W.R.C.*
The generalised Lagrangian mean equation; turbulent channel flow and the aetiology of streamwise vortices*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 736*
1990. `
..13.0,11.1: pdf for scalar depending on prob dist of length scale - K's name omitted from final paper*
KOLOVANDIN, B.A.; SOSINOVICH, V.A.*
Allowance for many length scales in the description of turbulent mixing*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 748*
1990. `
..13.0: just so*
HANJALIC, K.*
Practical predictions by single-point closure methods --twenty years of experience*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 762*
1990. `
..17.1,13.0,14.0: k, eps. and stress transport - expts suggest log law fails at high freq.*
COUSTEIX, J.; HOUDEVILLE, R.*
Modelling of unsteady boundary layers*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 782*
1990. `
..14.0: just so*
FERZIGER, J.H.; ET AL.*
Zonal modelling of turbulent flows - philosophy and accomplishments*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 800*
1990. `
..13.0: two-component limit*
LAUNDER, B.E.; TSELEPIDAKIS, D.P.*
Contribution to the second-moment modeling of sublayer turbulent transport*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 818*
1990. `
..11.4,05.0:just so*
SUZUKI, K.*
Heat and mass transfer and turbulence structure in the near wall region - prediction by single-point closure methods and some experimental data*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 853*
1990. `
..01.1,05.0,29.6: review - claims agreement between VITA and level, at least on burst interval*
TIEDERMAN, W.G.*
Eulerian detection of turbulent bursts*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 874*
1990. `
..01.1,05.0: not techniques - connection between near-wall VITA events and long time statistics*
ALFREDSSON, P.H.; JOHANSSON, A.V.*
The art of detection of turbulence structures*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 888*
1990. `
..32.2: wall meas. and probes*
KASHINSKY, O.N.*
Electrochemical method for studying local structure of turbulent flows*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 897*
1990. `
..01.1: uses udu/dt*
FALCO, R.E.; GENDRICH, C.P.*
The turbulence burst detection algorithm of Z. Zaric*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 911*
1990. `
..19.2,12.1,54.0: nine-sensor probe*
BALINT, J.L.; VUKOSLAVCEVIC, P.; WALLACE, J.M.*
The transport of enstrophy in a turbulent boundary layer*
Near-wall Turbulence - 1988 Zaric Memorial Conf. (S.J. Kline and N.H. Afgan, eds.), Hemisphere, p. 932*
1990. `
..25.6,05.0: the successful maggot*
JIMENEZ, J.; MOIN, P.*
The minimal flow unit in near wall turbulence*
CTR Manuscript 105*
1990. `
..16.2: circumf. vel. only*
HUMPHREY, J.A.C.; ET AL.*
On the flow in the unobstructed space between shrouded corotating disks*
Submitted to Phys. Fluids A (unpublished?)*
1990. `
..45.0,17.1,59.2: bimodal -- frequency much lower than eddy passage frequency*
DEVENPORT, W.J.; SIMPSON, R.L.*
Time-dependent and time-averaged turbulence structure near the nose of a wing-body junction*
J. Fluid Mech. 210, 23*
1990. `
..42.3,30.3: open circuit wind tunnel -- detailed scaling of results. Pr matters, but Re, lambda less than 50*
LIENHARD V, J.H.; VAN ATTA, C.W.*
The decay of turbulence in thermally stratified flow*
J. Fluid Mech. 210, 57*
1990. `
..24.2,53.0: leads to oblique waves with same spanwise wavelength as Gortler*
MALIK, M.R.; HUSSAINI, M.Y.*
Numerical simulation of interactions between Gortler vortices and Tollmien-Schlichting waves*
J. Fluid Mech. 210, 183*
1990. `
..20.0,02.1: double rollers are part of horseshoes -- which typically appear in groups of about 3*
FERRE, J.A.; MUMFORD, J.C. ET AL*
Three-dimensional large-eddy motions and fine-scale activity in a plane turbulent wake*
J. Fluid Mech. 210, 371*
1990. `
..53.0,05.0,45.0: more complicated than expected from streamline curvature effects*
ANWER, M.; SO, R.M.C.*
Frequency of sublayer bursting in a curved bend*
J. Fluid Mech. 210, 415*
1990. `
..05.0,01.1: z-wise rake -- burst, shear layer and sweep tend to occur in that temporal order*
ANTONIA, R.A.; BISSET, D.K.*
Spanwise structure in the near-wall region of a turbulent boundary layer*
J. Fluid Mech. 210, 437*
1990. `
..24.1: maximum Reynolds number of 20000 based on vorticity thickness*
HUANG, L.-S.; HO, C.-M.*
Small-scale transition in a plane mixing layer*
J. Fluid Mech. 210, 475*
1990. `
..53.0,24.4: can add or cancel*
MATSSON, O.J.E.; ALFREDSSON, P.H.*
Curvature and rotation-induced instabilities in channel flow*
J. Fluid Mech. 210, 537*
1990. `
..24.2,59.0: calcs for axi. and non-axi. linear disturbances*
KIM, I.; PEARLSTEIN, A.J.*
Stability of the flow past a sphere*
J. Fluid Mech. 211, 73*
1990. `
..50.0,44.2,59.0: relevance to blade wakes -- digitized video of bubbles, and  surface p. fluctuations*
GURSUL, I.; ROCKWELL, D.*
Vortex street impinging upon an elliptical leading edge*
J. Fluid Mech. 211, 211*
1990. `
..54.0: LDA in water -- intensity largest near core even after removing axial jitter*
GLEZER, A.; COLES, D.*
An experimental study of a turbulent vortex ring*
J. Fluid Mech. 211, 243*
1990. `
..18.2: gradual p. rise  -- large-scale structures unaffected in shape, but intensity and length scale increase.  Bulk compression seems to act without lag*
FERNANDO, E.M.; SMITS, A.J.*
A supersonic turbulent boundary layer in an adverse pressure gradient*
J. Fluid Mech. 211, 285*
1990. `
..54.0: just so*
HOPFINGER, E.J.; LINDEN, P.F.*
The effect of background rotation on fluid motions - a report on Euromech 245*
J. Fluid Mech. 211, 417*
1990. `
..53.0: says mean flow recovers quicker than turbulence*
ALVING, A.E.; SMITS, A.J.; WATMUFF, J.H.*
Turbulent boundary-layer relaxation from convex curvature*
J. Fluid Mech. 211, 529*
1990. `
..62.0: offset matters, dimensionally, as well as diameter*
KELLER, J.B.*
On unsymmetrically impinging jets*
J. Fluid Mech. 211, 653*
1990. `
..25.7: Euler solutions depend on numerics*
RHODES, J.A.; VON LAVANTE, E.*
Comparison of inviscid and viscous separated flows*
AIAA J. 28, 394*
1990. `
..02.0,17.1: flow viz. near nozzle of normal rectangular jet, aspect ratio 10 -- unsteady*
KROTHAPALLI, A.; LOURENCO, L.; BUCHLIN, J.M.*
Separated flow upstream of a jet in a crossflow*
AIAA J. 28, 414*
1990. `
..24.1,18.2: convective M of 0 . 51 and 0 . 64 -- LDV turbulence meas. scale on U1-U2, and Ruv is nearly 0 . 5*
SAMIMY, M.; ELLIOTT, G.S.*
Effects of compressibility on the characteristics of free shear layers*
AIAA J. 28, 439*
1990. `
..56.0,59.0: scale on tau, max. and k.delta -- semi-log region in backflow*
SIMPSON, R.L.; AGARWAL, N.K.; NAGABUSHANA, K.A.; OLCMEN, S.*
Spectral measurements and other features of separating turbulent flows*
AIAA J. 28, 446*
1990. `
..14.0,54.0: k, eps. and ASM predictions of Wood's flow*
ARMFIELD, S.W.; CHO, N.-H.; FLETCHER, C.A.J.*
Prediction of turbulence quantities for swirling flow in conical diffusers*
AIAA J. 28, 453*
1990. `
..06.0: also depends on slope of windward surface*
SIGAL, A.; DANBERG, J.E.*
New correlation of roughness density effect on the turbulent boundary layer*
AIAA J. 28, 554*
1990. `
..31.1: uses identity connecting shear-stress gradient and velocity-vorticity product*
ANTONIA, R.A.; RAJAGOPALAN, S.*
Performance of lateral vorticity probe in a turbulent wake*
Expts. in Fluids 9, 118*
1990. `
..32.2,29.6: good spatial resolution of conc. of fluorescent tracer*
GASKEY, S.; VACUS, P.; DAVID, R.; VILLERMAUX, J.*
A method for the study of turbulent mixing using fluorescence spectroscopy*
Expts. in Fluids 9, 137*
1990. `
..32.1: For measuring size and velocity of spherical particles - Erlangen work*
SELLENS, R.W.*
A compact, laser diode based phase Doppler system*
Expts. in Fluids 9, 153*
1990. `
..02.2,29.6,42.1: 7 mW laser beam scanned by square plex. block - mentions Oster-Yamamoto two-bucket technique for getting linear stratification. No mention of Sc*
DE SILVA, I.P.D.; MONTENEGRO, L.; FERNANDO, H.J.S.*
Measurement of interfacial distortions at a stratified entrainment interface*
Expts. in Fluids 9, 174*
1990. `
..31.1: eight prongs -- avoids ambiguities of 3-wire probe*
DOBBELING, K.; LENZE, B.; LEUCKEL, W.*
Computer-aided calibration and measurements with a quadruple hotwire probe*
Expts. in Fluids 8, 257*
1990. `
..24.1,18.2: convective M up to 0 . 45 -- meas. of u, v, and uv. Dussauge 92 says Mc = 0 . 2 not f.d.*
GOEBEL, S.G.; DUTTON, J.C.; KRIER, H.; RENIE, J.P.*
Mean and turbulent velocity measurements of supersonic mixing layers*
Expts. in Fluids 8, 263*
1990. `
..29.5: still low*
PY, B.*
Improvement in the frequency response of the electrochemical wall shear stress meter*
Expts. in Fluids 8, 281*
1990. `
..51.0,53.0,11.3: sequel to Dakos, 1984, on convex wall*
OKAMOTO, S.; GIBSON, M.M.*
Measurements in a heated turbulent wall jet on a concave wall*
Expts. in Fluids 8, 291*
1990. `
..31.2: multiple random calibration points and curve fit for everthing including wire T*
CIMBALA, J.M.; PARK, W.J.*
A direct hot-wire calibration technique to account for ambient temperature drift in incompressible flow*
Expts. in Fluids 8, 299*
1990. `
 ..13.0,16.1: just so*
BERG, B. v.d.*
Turbulence modeling - survey of activities in Belgium and the Netherlands, an appraisal of the status and a view on the prospects*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..13.0,22.2: personal view, then RAE/ UMIST /Harwell /QMC /Surrey*
LILLEY, G.M.*
A UK view on turbulence models for turbulent shear flow calculations*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..13.0,16.1: 3D Johnson-King, etc.*
KAYNAK, U.*
Computational turbulence studies in Turkey*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..14.0,09.0,11.6: two-phase, constant-property reaction, k, eps, and Baldwin-Lomax*
DOPAZO, C.; ALIOD, R.; VALINO, L.*
Turbulent flow modelling in Spain.  Overview and Developments*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..18.1,15.0: good review -- mainly simple models*
COUSTEIX, J.*
Calculation of turbulent compressible flows*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..13.0,14.0: useful review, especially of near-wall k, eps.*
RODI, W.*
Some current approaches in turbulence modelling*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..13.0,22.2: just so*
BRADSHAW, P.*
Collaborative testing of turbulence models*
AGARD Fluid Dynamics Panel, Advisory Rept 291*
1990. `
..22.2,12.1: nice review - includes sonnet by Corrsin*
GEORGE, W.K.*
The nature of turbulence*
To be presented at ASME Fluids Engg. Conf., Toronto*
1990. `
..53.0,09.5: see AIAA J. 27, 274*
BANDYOPADHYAY, P.R.*
Convex curvature concept of viscous drag reduction*
AIAA Prog. in Aero. and Astro vol. 123, Viscous drag reduction in boundary layers (D.M. Bushnell and J.N. Hefner, eds.), p. 285*
1990. `
..14.0,18.1: several models including Goldberg backflow model*
NUSCA, M.J.; CHAKRAVARTHY, S.R.; GOLDBERG, U.C.*
Computational fluid dynamics capability for the solid-fuel ramjet projectile*
J. Prop. Power 6, 256*
1990. `
..25.10,44.2: moving grids, Baldwin-Lomax*
RAI, M.M.; DRING, R.P.*
Navier-Stokes analyses of the redistribution of inlet temperature distortions in a turbine*
J. Prop. Power 6, 276*
1990. `
..24.1: vortices in untripped flow - then forcing*
BELL, J.H.; MEHTA, R.D.*
Effects of streamwise vorticity injection on turbulent mixing layer development*
AIAA Paper 90-1459*
1990.`
..45.0: see Devenport - secondary plus horseshoe vortex - turb. meas. but no vw*
CHANG, P.S.*
Experimental investigation of flow about a strut-endwall configuration*
AIAA Paper 90-1541*
1990. `
..19.2,20.0: Re, lambda up to 25 - unsurprisingly, no inertial subrange. SV has.*
THORODDSEN, S.T.; VAN ATTA, C.W.*
Experiments on small-scale anisotropy and dissipation in stably stratified turbulence*
UCSD paper for Phys. Fluids*
1990. `
..14.0,06.0: k, eps, with body-fitted grid - partly supported by Chrysler*
PARAMESWARAN, S.; CHOK, C.V.*
Numerical investigation of heat transfer and friction of rib-roughened channel*
Submitted to ASME Winter Annual Meeting*
1990. `
..25.10,44.2: Baldwin-Lomax model*
RAI, M.M.; MADAVAN, N.K.*
Computational analysis of rotor-stator interaction in turbomachinery using zonal techniques*
To appear in Progress in Aero. & Astro. 125*
1990. `
..29.6: useful review of biacetyl*
HERMANSON, J.C.; WINTER, M.*
Laser-induced fluorescence imaging of supersonic shear flow*
AIAA 90-0501*
1990. `
..30.3: f.s.t. too low to measure*
PATEL, V.C.*
Design and construction of the 1.8m x 1.5m low-turbulence wind tunnel*
IIHR Limited Distribution Report 170, University of Iowa*
1990. `
..59.0: rectangular section, Re about 1000*
MANSINGH, V.; OOSTHUIZEN, P.H.*
Effects of splitter plates on the wake flow behind a bluff body*
AIAA J. 28, 778*
1990. `
..62.0: two circular jets at 45 deg. - no ground*
RHO, B.J.; KIM, J.K.; DWYER, H.A.*
Experimental study of a turbulent cross jet*
AIAA J. 28, 784*
1990. `
..25.5,44.2,25.10: Baldwin-Lomax for turbomachines*
CHIMA, R.V.; YOKOTA, J.W.*
Numerical analysis of three-dimensional viscous internal flows*
AIAA J. 28, 798*
1990. `
..27.1: Pratt and Whitney work - streamwise p.g. from a coarse-grid Euler calc.*
KUNZ, R.F.; RHIE, C.M.; MALECKI, R.E.*
Calculation of internal flows using a single-pass, parabolized Navier-Stokes analysis*
AIAA J. 28, 817*
1990. `
..59.0,59.2: single spoiler*
NELSON, C.F.; KOGA, D.J.; EATON, J.K.*
Unsteady, separated flow behind an oscillating, two-dimensional spoiler*
AIAA J. 28, 845*
1990. `
..30.2: Langley 0 . 3m TCT - 0 . 7 percent rms vel. and some plenum reasonances*
NG, W.F.; GUNDAPPA, M.; GRIFFITH, D.O.; PETERSON, J.B.*
Turbulence measurements and noise generation in a transonic cryogenic wind tunnel*
AIAA J. 28, 853*
1990. `
..59.2: Periodicity at high alpha - VPI work*
REDINIOTIS, O.K.; STAPOUNTZIS, H.; TELIONIS, D.P.*
Vortex shedding over delta wings*
AIAA J. 28, 944*
1990. `
..24.7: exponentially growing NS solution*
WALEFFE, F.*
On the three-dimensional instability of strained vortices*
Phys.  Fluids A2, 76*
1990. `
..19.2: sweeping is Lagrangian, wrongly contradicted by RNG*
NELKIN, M.; TABOR, M.*
Time correlations and random sweeping in isotropic turbulence*
Phys.  Fluids A2, 81*
1990. `
..13.0: see ack. of other work on p. 1503 - quadratic formula, with one independent constant, depends on invariants of stress tensor*
SARKAR, S.; SPEZIALE, C.G.*
A simple nonlinear model for the return to isotropy in turbulence*
Phys.  Fluids A2, 84*
1990. `
..24.1: Karhunen-Loeve -- 30 parameters*
SIROVICH, L.; KIRBY, M.; WINTER, M.*
An eigenfunction approach to large scale transitional structures in jet flow*
Phys.  Fluids A2, 127*
1990. `
..18.1: still no ref. to Sarkar*
ZEMAN, O.*
Dilatation dissipation - the concept and application in modeling compressible mixing layers*
Phys.  Fluids A2, 178*
1990. `
..13.0,11.1: tensor diffusivity of mass*
GIRIMAJI, S.S.; POPE, S.B.*
A diffusion model for velocity gradients in turbulence*
Phys.  Fluids A2, 242*
1990. `
..25.6,24.2: reversed energy cascade in early stages makes Smago.-type models excessively dissipative*
PIOMELLI, U.; ZANG, T.A.; SPEZIALE, C.G.; HUSSAINI, M.Y.*
On the large-eddy simulation of transitional wall-bounded flows*
Phys. Fluids A2, 257*
1990. `
..25.6: for 2D flow*
LEITH, C.E.*
Stochastic backscatter in a subgrid-scale model -  plane shear mixing layer*
Phys.  Fluids A2, 297*
1990. `
..24.4,24.1: Re, theta = 74 - rolls and braids*
LASHERAS, J.C.; MEIBURG, E.*
Three-dimensional vorticity modes in the wake of a flat plate*
Phys. Fluids A2, 371*
1990. `
..06.0,59.0,57.0: h, plus up to 100 - u' measurements only. Downstream effects increase rapidly with promoter size*
BULLOCK, K.J.; LAI, J.C.S.; WALKER, T.B.*
Flow measurements behind attached ring-type turbulence promoters*
Phys. Fluids A2, 390*
1990. `
..19.2,25.6: all the fault of Fourier or low-Re simulation? - see Meneveau, 1990, on wavelets*
DOMARADZKI, J.A.: ROGALLO, R.S.*
Local energy transfer and nonlocal interactions in homogeneous isotropic turbulence*
Phys. Fluids A2, 413*
1990. `
..02.1,07.0: matched asymptotic expansions - an eddy viscosity is implied by Eq. 48, but why?*
PHILLIPS, W.R.C.; RATNANATHER, J.T.*
The outer region of a turbulent boundary layer*
Phys. Fluids A2, 427*
1990. `
..24.1: triggered by spanwise-periodic heaters on splitter plate*
NYGAARD, K.J.; GLEZER, A.*
Core instability of the spanwise vortices in a plane mixing layer*
Phys. Fluids A2, 461*
1990. `
..43.2,59.0: SF6 - big changes in vortex shedding*
OHYA, Y.; NAKAMURA, Y.*
Near wakes of a circular cylinder in stratified flows*
Phys. Fluids A2, 481*
1990. `
..19.2,12.2: potential part of omega x u much large than solenoidal part - not quite saying that p. gradient dominates?*
TSINOBER, A.*
On one property of Lamb vector in isotropic turbulent flow*
Phys. Fluids A2, 484*
1990. `
..43.2: 256 x 256 simulation - NCAR work*
McWILLIAMS, J.C.*
A demonstration of the suppression of turbulent cascades by coherent vortices in two-dimensional turbulence*
Phys. Fluids A2, 547*
1990. `
..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. `
..25.5: unsteady 2D calculation fails to reproduce unsteadiness of real 3D flow*
KOSEFF, J.R.; PRASAD, A.K.; PERNG, C.; STREET, R.L.*
Complex cavities - are two dimensions sufficient for computation?*
Phys. Fluids A2, 619*
1990. `
..05.0,01.1: significant probability of non-zero w at maxima of uv*
CHOI, W.C.; GUEZENNEC, Y.G.*
On the asymmetry of structure in turbulent boundary layers*
Phys. Fluids A2, 628*
1990. `
..59.0,25.5: input only the mean flow, and the vortex street grows*
TRIANTAFYLLOU, G.S.; KARNIADAKIS, G.E.*
Computational reducibility of unsteady viscous flows*
Phys. Fluids A2, 653*
1990. `
..29.6: includes survey of photochromic materials - see also thesis*
AGUI GARCIA, J.C.; HESSELINK, L.*
Application of holography to the measurement of velocity gradients in fluid flows sensitized with photochromic dyes*
Phys. Fluids A2, 688*
1990. `
..11.6: forced laminar calcs.*
MAHALINGAM, S.; CANTWELL, B.J.; FERZIGER, J.H.*
Full numerical simulation of coflowing, axisymmetric jet diffusion flames*
Phys. Fluids A2, 720*
1990. `
..24.7,25.3: no - see Buttke, Phys. Fluids A 1, 1283, 1989*
DRITSCHEL, D.G.; McINTYRE, M.E.*
Does countour dynamics go singular?*
Phys. Fluids A2, 748*
1990. `
..12.2,61.1,16.1: P, Q and R - a vortex is defined as a region where the rate-of-deformation tensor has complex eigenvalues*
CHONG, M.S.; PERRY, A.E.; CANTWELL, B.J.*
A general classification of three-dimensional flow fields*
Phys. Fluids A2, 765*
1990. `
..59.0,23.0: mean and fluctuating p and skin friction up to Re = 100000*
YOKUDA, S.; RAMAPRIAN, B.R.*
The dynamics of flow around a cylinder at subcritical Reynolds numbers*
Phys. Fluids A2, 784*
1990. `
..12.2,29.6: goes logarithmically to 3 at infinite Schmidt number - good discussion of details*
PRASAD, R.R.; SREENIVASAN, K.R.*
The measurement and interpretation of fractal dimensions of the scalar interface in turbulent flows*
Phys. Fluids A2, 792*
1990. `
..48.0: new experiment - region is wider than Dean and Bradshaw found*
TEITEL, M.; ANTONIA, R.A.*
The interaction region of a turbulent duct flow*
Phys. Fluids A2, 808*
1990. `
..19.3: intermittency of dissipation*
NOVIKOV, E.A.*
The effects of intermittency on statistical characteristics of turbulence and scale similarity of breakdown coefficients*
Phys. Fluids A2, 814*
1990. `
..59.0: intermittent recirculation due to surface roller*
YEH, H.H.; MOK, K.-M.*
On turbulence in bores*
Phys. Fluids A2, 821*
1990. `
..19.3: high-k structure is probably a pair of oppositely-oriented vortex sheets*
NAKANO, T.*
A microscopic vortical structure in fully developed turbulence*
Phys. Fluids A2, 829*
1990. `
..18.1,14.0: eddy viscosity result - equations for mean-square density fluctuation, TKE and a sort of dissipation*
YOSHIZAWA, A.*
Three-equation modeling of inhomogeneous compressible turbulence based on a two-scale direct-interaction approximation*
Phys. Fluids A2, 838*
1990. `
..29.6,22.1: large if beam lines up with with hairpins*
TRUMAN, C.R.; LEE, M.J.*
Effects of organized turbulence structures on the phase distortion in a coherent optical beam propagating through a turbulent shear flow*
Phys. Fluids A2, 851*
1990. `
..50.0,59.0: it increases the fractal dimension of low-Re cylinder wakes*
SCHNEIDER, S.P.*
Free-stream turbulence -  a limitation on fractal description of open-flow systems*
Phys. Fluids A2, 869*
1990. `
..22.2: 1945 onwards (Batchelor 70th birthday volume)*
TOWNSEND, A.A.*
Early days of turbulence research in Cambridge*
J. Fluid Mech. 212, 1*
1990. `
..22.2: G.K. Batchelor*
CRIGHTON, D.G.*
GKB and Euromech*
J. Fluid Mech. 212, 7*
1990. `
..24.2: stable at any Re for aspect ratio less than 3 . 2*
TATSUMI, T.; YOSHIMURA, T.*
Stability of the laminar flow in a rectangular duct*
J. Fluid Mech. 212, 437*
1990. `
..24.2: "breakthough" modes*
BARENBLATT, G.I.*
On a model of laminar-turbulent transition*
J. Fluid Mech. 212, 487*
1990. `
..12.2: "heuristic method for estimating certain features of slowly changing turbulent flows"*
HUNT, J.C.R.; CARRUTHERS, D.J.*
Rapid distortion theory and the "problems" of turbulence*
J. Fluid Mech. 212, 497*
1990. `
..11.1: mean-square fluctuation a quadratic function of mean concentration - not a gradient relation*
CHATWIN, P.C.; SULLIVAN, P.J.*
A simple and unifying physical interpretation of scalar fluctuation measurements from many turbulent shear flows*
J. Fluid Mech. 212, 533*
1990. `
..43.2,62.0: heavy upward-blowing jet, or conversely*
BAINES, W.D.; TURNER, J.S.; CAMPBELL, I.H.*
Turbulent fountains in an open chamber*
J. Fluid Mech. 212, 557*
1990. `
..05.0: short nonlinear phase then linear quasi-inviscid interaction with mean shear*
LANDAHL, M.T.*
On sublayer streaks*
J. Fluid Mech. 212, 593*
1990. `
..56.0: including negative skin friction - axisymmetric body*
DENGEL, P.; FERNHOLZ, H.H.*
An experimental investigation of an incompressible turbulent boundary layer in the vicinity of separation*
J. Fluid Mech. 212, 615*
1990. `
..43.0,11.3: 3-layer model for large z/L*
KADER, B.A.; YAGLOM, A.M.*
Mean fields and fluctuation moments in unstably stratified turbulent boundary layers*
J. Fluid Mech. 212, 637*
1990. `
..12.2,24.4,59.2: nonlinear interaction of natural and strip-heater-forced frequencies - not global turbulence*
WILLIAMS-STUBER, K.; GHARIB, M.*
Transition from order to chaos in the wake of an aircraft*
J. Fluid Mech. 213, 29*
1990. `
..42.3: useful review and new high-Sc experiments*
GOLDSTEIN, R.J.; CHIANG, H.D.; SEE, D.L.*
High-Rayleigh-number convection in a horizontal enclosure*
J. Fluid Mech. 213, 111*
1990. `
..12.2,11.1: eccentric annuli*
SWANSON, P.D.; OTTINO, J.M.*
A comparative computational and experimental study of chaotic mixing of viscous fluids*
J. Fluid Mech. 213, 227*
1990. `
..03.0: conditional patterns extend further out as Re decreases*
ANTONIA, R.A.; BISSET, K.K.; BROWNE, L.W.B.*
Effect of Reynolds number on the topology of the organized motion in a turbulent boundary layer*
J. Fluid Mech. 213, 267*
1990. `
..43.2,53.0: horizontal component of rotation vector produces streamline curvature effects - no vortex rolls*
COLEMAN, G.N.; FERZIGER, J.H.; SPALART, P.R.*
A numerical study of the turbulent Ekman layer*
J. Fluid Mech. 213, 313*
1990. `
..09.3,02.2: warm wall and tandem manipulators*
CHANG, S.-I.; BLACKWELDER, R.F.*
Modification of large eddies in turbulent boundary layers*
J. Fluid Mech. 213, 419*
1990. `
..20.0,50.0: airfoil with injection - cannot be unique*
CIMBALA, J.M.; PARK, W.J.*
An experimental investigation of the turbulent structure in a two-dimensional momentumless wake*
J. Fluid Mech. 213, 479*
1990. `
..24.1: density ratio as low as 0 . 45*
MONKEWITZ, P.A.; BECHERT, D.W.; BARSIKOW, B.; LEHMANN, B.*
Self-excited oscillations and mixing in a heated round jet*
J. Fluid Mech. 213, 611*
1990. `
..29.6: radon transform*
WATT, D.W.; VEST, C.M.*
Turbulent flow visualization by interferometric integral imaging and computed tomography*
Expts. in Fluids 8, 301*
1990. `
..47.2: Wigley double model - second and third order mean products*
PATEL, V.C.; SARDA, O.P.*
Mean-flow and turbulence measurements in the boundary layer and wake of a ship double model*
Expts. in Fluids 8, 319*
1990. `
..31.1: y-wise pulsing wire fixed, z-wise receiver wires traversed on vertical prongs.  See next*
DEVENPORT, W.J.; EVANS, G.P.; SUTTON, E.P.*
A traversing pulsed-wire probe for velocity measurements near a wall*
Expts. in Fluids 8, 336*
1990. `
..31.1: z-wise pulsing wire - whole probe head traversed*
CASTRO, I.P.; DIANAT, M.*
Pulsed wire velocity anemometry near walls*
Expts. in Fluids 8, 343*
1990. `
..29.6: coloured chalk and kerosene*
LU, F.K.; SETTLES, G.S.*
Color surface-flow visualization of fin-generated shock wave boundary-layer interactions*
Expts. in Fluids 8, 352*
1990. `
..32.1: in weakly 3D flow where hot wires are accurate*
MEHTA, R.D.*
Verification of three-dimensional laser Doppler velocimeter measurements*
Expts. in Fluids 8, 354*
1990. `
..04.0,59.2: chord Re 140,000 - mean flow only*
FITZGERALD, E.J.; MUELLER, T.J.*
Measurements in a separation bubble on an airfoil using laser velocimetry*
AIAA J. 28, 584*
1990. `
..13.0,11.1: realizability - and assumption that time-scale ratio tends to a constant for scalar dissipation equation*
SHIH, T.-H.; LUMLEY, J.L.; CHEN, J.-Y.*
Second-order modeling of a passive scalar in a turbulent shear flow*
AIAA J. 28, 610*
1990. `
..24.1,25.6: but why does linear theory work?*
SANDHAM, N.D.; REYNOLDS, W.C.*
Compressible mixing layer - linear theory and direct simulation*
AIAA J. 28, 618*
1990. `
..25.5: driven cavity - linearized approx., but improvement on exponential scheme*
KARKI, K.C.; PATANKAR, S.V.; MONGIA, H.C.*
Three-dimensional fluid flow calculations using a flux-spline method*
AIAA J. 28, 631*
1990. `
..59.2,59.0: vortex street and the rest*
DEGANI, D.; ZILLIAC, G.G.*
Experimental study of nonsteady asymmetric flow around an ogive-cylinder at incidence*
AIAA J. 28, 642*
1990. `
..59.0,11.3,14.0: strongly anisotropic, contradicting k, eps. model *
ROE, L.A.; PROCTOR, C.L.*
Velocity measurements in a turbulent centerbody diffusion flame*
AIAA J. 28, 655*
1990. `
..14.0,54.0: standard k, eps. not bad*
KHODADADI, J.M.; VLACHOS, N.S.*
Effects of turbulence model constants on computation of confined swirling flows*
AIAA J. 28, 750*
1990. `
..50.0: k, eps. calcs, show reasonable agreement with experiment*
LIOU, T.-M.; WU, S.-M.; HWANG, Y.-H.*
Experimental and theoretical investigations of turbulent flow in a side-inlet rectangular combustor*
J. Prop. Power 6, 131*
1990. `
..44.2: just so*
HSU, C.T.; MINACHI, A.*
Performance tests of tornado-type wind turbine models*
J. Prop. Power 6, 181*
1990. `
..61.0: semi-cylinder plus fairing - single large vortex dominates*
PIERCE, F.J.; TREE, I.K.*
The mean flow structure on the symmetry plane of a turbulent junction vortex*
J. Fluids Engg. 112, 16*
1990. `
..14.0: correct limiting behaviour of damping of epsilon*
NAGANO, Y.; TAGAWA, M.*
An improved k, eps. model for boundary layer flows*
J. Fluids Engg. 112, 33*
1990. `
..14.0: including mod. for adverse pg. - but "fundamental inadequacy"*
DE HENAU, V.; RAITHBY, G.D.; THOMPSON, B.E.*
Prediction of flows with strong curvature and pressure gradient using the k-eps. turbulence model*
J. Fluids Engg. 112, 40*
1990. `
..09.2: including spectra*
WANG, S.K.; ET AL.*
Statistical analysis of turbulent two-phase pipe flow*
J. Fluids Engg. 112, 89*
1990. `
..09.2: predicts near wall concentration in upflow*
LOPEZ DE BERTODANO, M.; ET AL.*
The prediction of two-phase turbulence and phase distribution phenomena using a Reynolds stress model*
J. Fluids Engg. 112, 107*
1990. `
..11.3,62.0: single jet - St and stresses but no vw*
SUBRAMANIAN, C.S.; LIGRANI, P.M.; ET AL.*
Development and structure of a film-cooling jet in a turbulent boundary layer with heat transfer*
Presented at Third Int. Sympo. on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu (Publisher??)*
1990. `
..28.1,25.1:especially Hartley, but including Walsh, Radon and FFT history*
BRACEWELL, R.N.*
Numerical transforms*
Science 248, 697, 11 May*
1990. `
..07.1,12.1:Re, theta up to 39000 - U and u from LDV. In IFP Lib.*
PETRIE, H.L.; FONTAINE, A.A.; SOMMER, S.T.; BRUNGART, T.A.*
Large flat plate turbulent boundary layer evaluation*
Penn. State Univ. ARL Tech. Memo. 89-207*
1990. `
..28.2,22.2: are computer languages created in the image of the language spoken by their makers - and if so did the inventors of Basic speak pidgin English?*
PETTERSEN, R.H.*
The tongues of men and machines*
Byte vol. 15, no. 8, p. 356*
1990. `
..25.2,25.5: symmetric solution is accurate but unstable to perturbations in real life*
ANDERSON, C.R.; ET AL*
On the accurate calculation of vortex shedding*
Phys.  Fluids A2, 883*
1990. `
..19.2,12.2: fractal properties evaluated from 128^3 simulation*
HOSOKAWA, I.; YAMAMOTO, K.*
Intermittency exponents and generalized dimensions of a directly simulated fully developed turbulence*
Phys.  Fluids A2, 889*
1990. `
..24.1,18.1: definition same as Papamoschou if two streams have same gamma*
JACKSON, T.L.; GROSCH, C.E.*
Absolute/convective instabilities and the convective Mach number in a compressible mixing layer*
Phys.  Fluids A2, 949*
1990. `
..25.6,19.2: comment on Lesieur and Rogallo closure with "hyperviscosity" -- k-dependent viscosity*
HERRING, J.R.*
Comparison of closure to spectral-based large eddy simulations*
Phys.  Fluids A2, 979*
1990. `
..09.0: simulations -- particles collect in regions of high strain rate*
SQUIRES, K.D.; EATON, J.K.*
Particle response and turbulence modification in isotropic turbulence*
Phys.  Fluids A2, 1191*
1990. `
..24.1,18.2: Reynolds stresses decrease at least up to convective Mach no. of 0 . 86*
ELLIOT, G.S.; SAMIMY, M.*
Compressibility effects in free shear layers*
Phys.  Fluids A2, 1231*
1990. `
..08.0: average period of bursts and ejections is increased by suction*
ANTONIA, R.A.; BISSET, D.K.; ET AL.*
Effect of wall suction on bursting in a turbulent boundary layer*
Phys.  Fluids A2, 1241*
1990. `
..13.0: leads to a length or time scale*
POPE, S.B.; CHEN, Y.L.*
The velocity-dissipation probability density function model for turbulent flows*
Phys.  Fluids A2, 1437*
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. `
..05.0: for y, plus less than 10, instantaneous vorticity always has sign of mean*
KLEWICKI, J.C.; GENDRICH, C.P.; ET AL.*
On the sign of the instantaneous spanwise vorticity component in the near-wall region of turbulent boundary layers*
Phys.  Fluids A2, 1497*
1990. `
..13.0,12.2: small realizable region for linear pressure-strain model and RDT gives a poor result*
SHIH, T.-H.; REYNOLDS, W.C.; MANSOUR, N.N.*
A spectrum model for weakly anisotropic turbulence*
Phys.  Fluids A2, 1500*
1990. `
..14.0,54.0: standard k, eps. overpredicts decay of Pauley and Eaton's vortices*
ZHU, J.X.; FIEBIG, M.; MITRA, N.K.*
Numerical simulation of a 3-D turbulent flow field with longitudinal vortices*
To be presented at ASME Winter Annual Meeting*
1990. `
..44.1,05.0,48.0: spacing 100 wall units for any strength of shear on the free surface*
RASHIDI, M.; BANERJEE, S.*
Streak characteristics and behavior near wall and interface in open channel flows*
J. Fluids Engg. 112, 164*
1990. `
..14.0: asymptotic solution gives log law plus divergent terms*
TAKEMITSU, N.*
An analytical study of the standard k, eps. model*
J. Fluids Engg. 112, 192*
1990. `
..14.0: nonlinear k, eps. or k, l model produces stress-induced secondary flow*
HUR, N.; THANGAM, S.; SPEZIALE, C.G.*
Numerical study of turbulent secondary flows in curved ducts*
J. Fluids Engg. 112, 205*
1990. `
..05.0,07.0: y^3 variation*
GRANVILLE, P.S.*
A near-wall eddy viscosity formula for turbulent boundary layers in pressure gradients suitable for momentum, heat, or mass transfer*
J. Fluids Engg. 112, 240*
1990. `
..14.0: multiscale and k, omega.  Fair agreement except with Brown*
WILCOX, D.C.*
Supersonic compression-corner applications of a multiscale model for turbulent flows*
AIAA J. 28, 1194*
1990. `
..25.1: quotes Rechenberg's work -- approach to pattern recognition*
HAJELA, P.*
Genetic search -- an approach to the nonconvex optimization problem*
AIAA J. 28, 1205*
1990. `
..42.3: buoyancy reversal*
SHY, S.S.; BREIDENTHAL, R.E.*
Laboratory experiments on the cloud-top entrainment instability*
J. Fluid Mech. 214, 1*
1990. `
..05.0: Gortler mechanism*
AIHARA, Y.*
Formation of longitudinal vortices in the sublayer due to boundary-layer turbulence*
J. Fluid Mech. 214, 111*
1990. `
..24.1,29.6: LDV synchronized with flow viz.*
PANIDES, E.; CHEVRAY, R.*
Vortex dynamics in a plane, moderate-Reynolds-number shear layer*
J. Fluid Mech. 214, 411*
1990. `
..19.2,54.0: mathematical -- real, non-Gaussian, non-linear turbulence is not time-reversal invariant*
DRUMMOND, I.T.; MUNCH, W.*
Turbulent stretching of line and surface elements*
J. Fluid Mech. 215, 45*
1990. `
..42.3: vortex-roll pairs can be lost by "pinching"*
SHADID, J.N.; GOLDSTEIN, R.J.*
Visualization of longitudinal convection roll instabilities in an inclined enclosure heated from below*
J. Fluid Mech. 215, 61*
1990. `
..05.0,56.0: small intermittent reversed-flow regions.  Spanwise wavelength still about 100 wall units*
LIAN, Q.X.*
A visual study of the coherent structure of the turbulent boundary layer in flow with adverse pressure gradient*
J. Fluid Mech. 215, 101*
1990. `
..54.0: infinitesimal sheets can develop curvature singularities instead of a finite vortex core*
BAKER, G.R.; SHELLEY, M.J.*
On the connection between thin vortex layers and vortex sheets*
J. Fluid Mech. 215, 161*
1990. `
..24.2,54.0: spanwise axis of rotation -- vortex rolls from longitudinal waves*
FINLAY, W.H.*
Transition to oscillatory motion in rotating channel flow*
J. Fluid Mech. 215, 209*
1990. `
..24.1,09.2: mixing layer behind fence -- cavitation in spanwise and streamwise vortices*
O'HERN, T.J.*
An experimental investigation of turbulent shear flow cavitation*
J. Fluid Mech. 215, 365*
1990. `
..42.3: sensitivity to initial conditions -- no direct evidence for internal waves.  Ri up to 10, and counter-gradient heat flux*
YOON, K.; WARHAFT, Z.*
The evolution of grid-generated turbulence under conditions of stable thermal stratification*
J. Fluid Mech. 215, 601*
1990. `
..13.0,11.2: measured third-order moments highly intermittent, with flatness factors of 80 or more.  All can be represented as combinations of u, v and skewness*
NAGANO, Y.; TAGAWA, M.*
A structural turbulence model for triple products of velocity and scalar*
J. Fluid Mech. 215, 639*
1990. `
..43.1,42.1: thermal convection on inclined plate*
SCHUMANN, U.*
Large-eddy simulation of the up-slope boundary layer*
Q.J. Roy. Met. Soc. 116, 637*
1990. `
..59.2,54.0: transient spanwise vortex -- flow viz and some hot wire measurements*
SWIRYDCZUK, J.*
A visualization study of the interaction of a free vortex with the wake behind an airfoil*
Expts. in Fluids 9, 181*
1990. `
..31.1: rapid azimuthal rotation in circular duct*
WARK, C.E.; NAGIB, H.M.; JENNINGS, M.J.*
A rotating hot-wire technique for spatial sampling of disturbed and manipulated duct flows*
Expts. in Fluids 9, 191*
1990. `
..59.0,61.0: telescope -- detailed measurements near change of diameter, plus discussion of vortex street*
KO, N.W.M.; CHAN, A.S.K.*
In the intermixing region behind circular cylinders with stepwise change of the diameter*
Expts. in Fluids 9, 213*
1990. `
..04.0,25.6: detailed comparisons with simulations -- wall-stress fluctuations of about 0 . 5 rms*
NIEDERSCHULTE, M.A.; ADRIAN, R.J.; HANRATTY, T.J.*
Measurements of turbulent flow in a channel at low Reynolds numbers*
Expts. in Fluids 9, 222*
1990. `
..59.0,44.3: need cylinder aspect ratio of 7 even with good endplates*
FOX, T.A.; WEST, G.S.*
On the use of end plates with circular cylinders*
Expts. in Fluids 9, 237*
1990. `
..09.0,24.4: general review*
CARPENTER, P.W.*
Status of transition delay using compliant walls*
Viscous Drag Reduction in Boundary Layers (D.M. Bushnell and J.N. Hefner, editors), AIAA Prog. Astro. & Aero. 123, 79*
1990. `
..29.2: including elliptical section static tubes*
ROSSOW, V.J.*
Probe systems for measuring time-averaged static pressure and turbulence intensity*
Submitted to AIAA J. of Aircraft*
1990. `
..29.2: dished-end pitot tubes -- inviscid calculations*
ROSSOW, V.J.*
Probe shapes that measure time-averaged streamwise momentum and cross-stream turbulence intensity*
Submitted to AIAA J. of Aircraft*
1990. `
..19.2: derivatives in x too large at Re, lambda up to 2800 in wind tunnel*
KUZNETSOV, V.R.; KARYAKIN, M.Y.; PRASKOVSKY, A.A.*
Anisotropy of turbulence fine-scale structure in high Reynolds number flows*
Presented at 3rd European Turbulence Conference, Stockholm*
1990. `
..13.0,18.1,24.1: compressible dissipation -- mentions Wilcox's finding that it fouls up BL*
SARKAR, S.; BALAKRISHNAN, L.*
Application of a Reynolds stress turbulence model to the compressible shear layer*
NASA CR 182002, ICASE Rpt. 90-18, AIAA-90-1465*
1990. `
..18.1: Aug. 1989 status review at Ames*
HARRIS, J.E.; MARVIN, J.G.; ERLEBACHER, G.; LIOU, M.-S.*
Turbulence modeling for hypersonic flows*
NASA TM 1114*
1990. `
..12.2,25.5: just so -- cover says "Introduction of chaos theory in CFD"*
PULLIAM, T.H.*
An introduction to chaos theory in CFD*
AIAA-90-1440*
1990. `
..13.0,28.1: spatial filtering/enhancing mainly for shock waves*
VOROZHTSOV, E.V.*
On the classification of discontinuities by the pattern recognition methods*
Computers and Fluids, 18, 35*
1990. `
..25.2,18.1: sensitivity analysis needed*
MEHTA, U.B.*
Some aspects of uncertainty in computing hypersonic flight estimates*
NASA TM 102804*
1990. `
..25.2,18.1: philosophy of CFD*
MEHTA, U.B.*
Computational requirements for hypersonic flight performance estimates*
AIAA J. Spacecraft 27, 103*
1990. `
..47.2,16.1: div (uX[uXomega])=0 approx.*
WIEGHARDT, K.*
On a characteristic of threedimensional free turbulence*
Ship Tech. Research/Schiffstechnik, 37, 35*
1990. `
..13.0,15.0: Stratford-Gadd or LRR for hills*
HUNT, J.C.R.; NEWLEY, T.M.J.; WENG, W.S.*
Analysis and computation of turbulent boundary layers with varying pressure gradients*
Computational Methods in Aeronautical Fluid Dynamics (P. Stow, ed. -- 1987 IMA Conf., Reading - in Terman), Oxford UP, p. 59*
1990. `
..27.1,25.5: abstract of Dedoussis, Koh, Ryou theses*
BRADSHAW, P.*
Nearly Navier-Stokes solutions*
Computational Methods in Aeronautical Fluid Dynamics (P. Stow, ed. -- 1987 IMA Conf., Reading - in Terman), Oxford UP, p. 59*
1990. `
..54.0: what is a vortex?*
LEVY, Y.; DEGANI, D.; SEGINER, A.*
Graphical visualization of vortical flows by means of helicity*
AIAA J. 28, 1347*
1990. `
..54.0,59.2: helicopter blade slap*
BOOTH, E.R.*
Experimental observations of two-dimensional blade-vortex interaction*
AIAA J. 28, 1353*
1990. `
..50.0,59.2: Re=140*
CIMBALA, J.M.; KREIN, M.V.*
Effect of freestream conditions on the far wake of a circular cylinder*
AIAA J. 28, 1369*
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. `
..25.5,25.8: finite-element Galerkin, akin to finite volume -- but 3 to 4 times the effort of structured meshes*
MAVRIPLIS, D.J.; JAMESON, A.*
Multigrid solution of the Navier-Stokes equations on triangular meshes*
AIAA J. 28, 1415*
1990. `
..16.1,13.0: published version*
ABID, R.; VATSA, V.N.; JOHNSON, D.A.; WEDAN, B.W.*
Prediction of separated transonic wing flows with nonequilibrium algebraic turbulence model*
AIAA J. 28, 1426*
1990. `
..15.0,18.1:law of the wall plus outer-layer eddy viscosity*
WAHLS, R.A.; BARNWELL, R.W.; DEJARNETTE, F.R.*
Defect stream function, law of the wall/wake method for compressible turbulent boundary layers*
AIAA J. 28, 1432*
1990. `
..45.0,54.0: see Gessner -- all Reynolds stresses measured but not all shown*
MIAU, J.J. ET AL*
Flow distortion in a circular-to-rectangular transition duct*
AIAA J. 28, 1447*
1990. `
..25.7: nominally time-accurate, but runs different parts of the field to different times*
DANNENHOFFER, J.F.; GILES, M.B.*
Accelerated convergence of Euler solutions using time inclining*
AIAA J. 28, 1457*
1990. `
..14.0: adjusted k, eps.*
CHAMPION, M.; LIBBY, P.A.*
 Stagnation streamline turbulence revisited*
AIAA J. 28, 1525*
1990. `
..29.6,24.1: details of PLIF*
PAUL, P.H.; VAN CRUYNINGEN, I.; HANSON, R.K.; KYCHAKOFF, G.*
High resolution digital flowfield imaging of jets*
Expts. in Fluids 9, 241*
1990. `
..31.3: Allen salt method updated*
SOKOLOV, M.; MASHAAL, M.*
Velocity measurements in slow flow by the conductance-tracer method*
Expts. in Fluids 9, 252*
1990. `
..29.6: all the usual traps and some new ones*
GURSUL, I.; LUSSEYRAN, D.; ROCKWELL, D.*
On interpretation of flow visualization of unsteady shear flows*
Expts. in Fluids 9, 257*
1990. `
..09.1: 1 . 5 percent mass loading of 80 micron particles*
ZOLTANI, C.K.; BICEN, A.F.*
Velocity measurements in a turbulent, dilute, two-phase jet*
AIAA J. 9, 295*
1990. `
..59.2,18.1: discusses a wide variety of schemes*
BUSHNELL, D.*
Supersonic aircraft drag reduction*
AIAA-90-1596*
1990. `
..13.0: transport equations for uv and k, but algebraic relation for dissipation and normal stresses*
GAFFNEY, R.L.; SALAS, M.D.; HASSAN, H.A.*
An abbreviated Reynolds stress turbulence model for airfoil flows*
AIAA-90-1468*
1990. `
..13.0: motivated by Johnson-King -- but non-iterative and therefore easier to put in an N-S solver*
AHMED, S.; TANNEHILL, J.*
Numerical prediction of turbulent flow over airfoil sections with a new nonequilibrium turbulence model*
AIAA-90-1469*
1990. `
..13.0,22.2: just so*
BRADSHAW, P.*
Progress in turbulence research*
AIAA-90-1480*
1990. `
..14.0: improved k, omega -- called k, tau*
SPEZIALE, C.G.; ABID, R.; ANDERSON, E.C.*
A critical evaluation of two-equation models for near wall turbulence*
AIAA-90-1481*
1990. `
..14.0: Lam-Bremhorst k, eps. variant, based partly on limiting behavior at y=0*
GOLDBERG, U.; OTA, D.*
A k-e near-wall formulation for separated flows*
AIAA-90-1482*
1990. `
..14.0: advantage over eps. is that kl equation is more robust*
SMITH, B.R.*
The k-kl turbulence model and wall layer model for compressible flows*
AIAA-90-1483*
1990. `
..45.0,50.0: shortened version of NASA CR 4188, 1988*
SHOHADAEE, A.; CRAWFORD, R.; HEDAYATPOUR, A.*
Influence of bulk turbulence and entrance boundary layer thickness on the curved duct flow field*
AIAA-90-1502*
1990. `
..13.0,50.0: LEIM does quite well on Hancock*
MURTHY, S.N.B.; HONG, S.K.*
Turbulent boundary layer with free stream turbulence*
AIAA-90-1503*
1990. `
..50.0,24.4: laminar-Tollmien-Schlichting waves studied by array of Radio Shack electret microphones. Flow speed 12 m/s*
KENDALL, J.M.*
Boundary layer receptivity to freestream turbulence*
AIAA-90-1504*
1990. `
..25.5: just so -- modified Steger-Warming*
MACCORMACK, R.W.*
Solution of the Navier-Stokes equations in three dimensions*
AIAA-90-1520*
1990. `
..25.5: incompressible -- Issa PISO algorithm better than SIMPLE for fine grid*
JIANG, Y.; CHEN, C.P.; TUCKER, P.K.*
Multigrid solution of unsteady Navier-Stokes equations using a pressure method*
AIAA-90-1522*
1990. `
..27.4: chord Reynolds number only 150000 -- NS solutions show odd wiggles*
NAKAMURA, Y.; JIA, W.; YASUHARA, M.*
A flow around airfoil with slat and flap*
AIAA-90-1535*
1990. `
..61.0,44.2: flow viz. and surface p. fluc. -- bimodal p.d.f. in CCNY 4x4 tunnel with no splitter plate*
AGUI, J.; ANDREOPOULOS, J.*
Experimental investigation of a three-dimensional boundary layer flow in the vicinity of an upright wall mounted cylinder*
AIAA-90-1545*
1990. `
..18.1,13.0,14.0: new pressure-strain term including dilatation*
LEE, J.; TAULBEE, D.B.; HOLDEN, M.S.*
A study of turbulence on a compression ramp with k-eps. and Reynolds stress models*
AIAA-90-1582*
1990. `
..54.0,56.0: vortex generators, jet and otherwise*
LIN, J.C.; HOWARD, F.G.; BUSHNELL, D.M.*
Investigation of several passive and active methods for turbulent flow separation control*
AIAA-90-1598*
1990. `
..30.4,49.0: porous walls with return-flow passage -- as for shock control*
RAGHUNATHAN, S.; McILWAIN, S.*
Wide angle diffusers with passive boundary-layer control*
AIAA-90-1600*
1990. `
..25.10,25.5: avoids points moving inside body -- transonic*
CONNETT, W.C.; ET AL.*
An adaptive-grid technique for the solution of Navier-Stokes equations*
AIAA-90-1605*
1990. `
..25.10: rapid prototyping -- main goal is to develop an extensible architecture.  Mt. View company*
CORDOVA, J.Q.*
VisualGrid -- A software package for interactive grid generation*
AIAA-90-1607*
1990. `
..01.1,05.0: black and white*
ROBINSON, S.K.*
A perspective on coherent structures and conceptual models for turbulent boundary layer physics*
AIAA-90-1638*
1990. `
..18.2: reflected shock in shock tube -- HWA and p' meas. Revised in Phys. Fluids A4, 2562, 1992*
HONKAN, A.; ANDREOPOULOS, J.*
Experiments in a shock wave/homogenous turbulence interaction*
AIAA-90-1647*
1990. `
..13.0,14.0: excellent review*
SPEZIALE, C.G.*
Analytical methods for the development of Reynolds stress closures in turbulence*
ICASE Rept 90-26*
1990. `
..02.2,12.2: swept laser sheet LIF in dye -- interface dimension 2 . 35*
PRASAD, R.R.; SREENIVASAN, K.R.*
Quantitative three-dimensional imaging and the structure of passive scalar fields in fully turbulent flows*
J. Fluid Mech. 216, 1*
1990. `
..11.3,50.0: asymmetry of pdf leads to countergradient heat flux*
VEERAVALLI, S.; WARHAFT, Z.*
Thermal dispersion from a line source in the shearless turbulent mixing layer*
J. Fluid Mech. 216, 35*
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. `
..54.0: bifurcating axi. Euler (S.L. Bragg-Hawthorne) solutions*
LEIBOVICH, S.; KRIBUS, A.*
Large-amplitude wavetrains and solitary waves in vortices*
J. Fluid Mech. 216, 459*
1990. `
..12.3: sublayer-like streaks -- so solid boundary not necessary.  RDT is a good approx.*
LEE, M.J.; KIM, J.; MOIN, P.*
Structure of turbulence at high shear rate*
J. Fluid Mech. 216, 561*
1990. `
..06.0,59.0: laminar -- roughness acts as a source of streamwise vorticity*
FLORYAN, J.M.; DALLMANN, U.*
Flow over a leading edge with distributed roughness*
J. Fluid Mech. 216, 629*
1990. `
..14.0: mixing length does not work in the outer layer -- use a one-equation model*
BELCHER, S.E.; WENG, W.S.; CARRUTHERS, D.J.; HUNT, J.C.R.*
The modelling of perturbed turbulent boundary layers*
Presented at 3rd European Turbulence Conf.*
1990. `
..13.0,14.0: RNG derivation of Yoshizawa quadratic*
RUBINSTEIN, R.; BARTON, J.M.*
Nonlinear Reynolds stress models and the renormalization group*
Phys. Fluids A2, 1472*
1990. `
..16.1,25.6: spanwise pressure gradient*
MOIN, P.; SHIH, T.-H.; DRIVER, D.; MANSOUR, N.N.*
Direct numerical simulation of three-dimensional turbulent boundary layer*
Phys. Fluids A2, 1846*
1990. `
..13.0: up to fourth order in anisotropy -- RDT based*
LEE, M.J.*
A contribution toward rational modeling of the pressure-strain-rate correlation*
Phys. Fluids A2, 630*
1990. `
..16.2: pressure gradient affects U, not W*
DRIVER, D.M.*
Experimental study of a three-dimensional shear-driven turbulent boundary layer with streamwise adverse pressure gradient*
NASA TM 102211, Stanford M.E. Dept. MD-57*
1990. `
..59.0,17.1: even square cylinders will autorotate*
SKEWS, B.W.*
Autorotation of rectangular plates*
J. Fluid Mech. 217, 33*
1990. `
..27.1,59.2,20.0: inner-wake width affected by outer-layer eddies and therefore by bulk Re - inactive motion*
NAKAYAMA, A.; LIU, B.*
The turbulent near wake of a flat plate at low Reynolds number*
J. Fluid Mech. 217, 93*
1990. `
..11.1,19.2: very high Pr theory, similar to DIA - see Phys. Fluids 1985, p. 1299*
QIAN, J.*
The spectrum of a turbulent passive scalar in the viscous-convective range*
J. Fluid Mech. 217, 203*
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. `
..59.0: effect of small downstream cylinder*
STRYKOWSKI, P.J.; SREENIVASAN, K.R.*
On the formation and suppression of vortex shedding at low Reynolds numbers*
J. Fluid Mech. 218, 71*
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. `
..05.0,09.1: u increases but v and uv decrease*
WALKER, D.T.; TIEDERMAN, W.G.*
Turbulent structure in a channel flow with polymer injection at the wall*
J. Fluid Mech. 218, 377*
1990. `
..05.0,06.0: just so*
PERRY, A.E.; LI, J.D.*
Experimental support for the attached-eddy hypothesis in zero-pressure-gradient turbulent boundary layers*
J. Fluid Mech. 218, 405*
1990. `
..20.0: opposed structures twice as frequent as alternating*
BISSET, D.K.; ANTONIA, R.A.; BROWNE, L.W.B.*
Spatial organization of large structures in the turbulent far wake of a cylinder*
J. Fluid Mech. 218, 439*
1990. `
..20.0,11.2: including temperature correlations*
BISSET, K.K.; ANTONIA, R.A.; BRITZ, D.*
Structure of large-scale vorticity in a turbulent far wake*
J. Fluid Mech. 218, 463*
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. `
..25.7: spurious lift - numerical double-valued solution?*
PULLIAM, T.H.*
Computational challenge - Euler solution for ellipses*
AIAA J. 28, 1703*
1990. `
..47.1: trailer for review - tends to an axi. wake*
LUEPTOW, R.M.*
Turbulent boundary layer on a cylinder in axial flow*
AIAA J. 28, 1705*
1990. `
..14.0,25.5: explicit finite-vol. scheme with local time-stepping - seems to overcome stiffness problem*
GEROLYMOS, G.A.*
Implicit multiple-grid solution of the compressible Navier-Stokes equations using k, eps. turbulence closure*
AIAA J. 28, 1707*
1990. `
..24.1: max. amplification rate correlates on convective Mach number*
ZHUANG, M.; KUBOTA, T.; DIMOTAKIS, P.E.*
Instability of inviscid, compressible free shear layer*
AIAA J. 28, 1728*
1990. `
..25.5: published version*
CHAVIAROPOULOS, P.; GIANNAKOGLOU, K.; PAPAILIOU, K.D.*
Novel scalar-vector potential formulation for three-dimensional, inviscid, rotational flow problems*
AIAA J. 28, 1734*
1990. `
..24.4,16.2: especially travelling waves - experiment*
BIPPES, H.; NITSCHKE-KOWSKY, P.*
Experimental study of instability modes in a three-dimensional boundary layer*
AIAA J. 28, 1758*
1990. `
..17.1,59.0: backflow velocity can exceed free stream value in highly unsteady cases*
AGARWAL, N.K.; SIMPSON, R.L.*
Backflow structure of steady and unsteady separating turbulent boundary layers*
AIAA J. 28, 1764*
1990. `
..43.1,05.0: and in rivers*
NARASIMHA, R.; KAILAS, S.V.*
Turbulent bursts in the atmosphere*
Atmos. Environment 24A, 1635*
1990. `
..18.1,13.0: just so - see TM X-622248, 1973*
RUBESIN, M.W.*
Extra compressibility terms for Favre-averaged two-equation models of inhomogeneous turbulent flows*
NASA Contractor Report 177556*
1990. `
..18.1,19.3:just so*
LEE, S.; LELE, S.K.; MOIN, P.*
Eddy-shocklets in decaying compressible turbulence*
CTR Manuscript 117*
1990. `
..44.2: advice on 4-blade cascades*
LANGSTON, L.S.*
Research on cascade secondary and tip-leakage flows - periodicity and surface flow visualization*
In AGARD CP 469, Secondary flows in turbomachines*
1990. `
..13.0,25.6: from ensembles of fluid particle paths from simulations*
BERNARD, P.S.; HANDLER, R.A.*
Reynolds stress and the physics of turbulent momentum transport*
NRL Memorandum Report 6685*
1990. `
..44.2: Dring and Joslyn on end walls, Langston on cascades*
ANON*
Secondary flows in turbomachines*
AGARD CP 469*
1990. `
..25.3: BIM - density equivalent to reciprocal of magnetic permittivity.  Overheads only*
HUNT, B.*
Generalized nonlinear boundary integral methods for compressible, viscous flows over arbitrary bodies - knowledge-based C.F.D.*
Presented at Japan/USA Boundary Elements Symposium, Palo Alto*
1990. `
..09.3: reduced production balanced by diffusion*
LEMAY, J.; DELVILLE, J.; BONNET, J.P.*
Turbulent kinetic energy balance in a LEBU modified turbulent boundary layer*
Expts. in Fluids 9, 301*
1990. `
..53.0,24.1: rolls appear after a noisy start - relevant to mixing layers?*
TAKEDA, Y.; KOBASHI, K.; FISCHER, W.E.*
Observation of the transient behaviour of Taylor vortex flow between rotating concentric cylinders after sudden start*
Expts. in Fluids 9, 317*
1990. `
..18.2,47.2: minimum at design Mach number*
LIEBENBERG, L.; BUNT, E.A.*
Wave drag coefficient of a model "Busemann biplane" catamaran*
Expts. in Fluids 9, 352*
1990. `
..49.0,54.0: plow-type vortex generator on inclined wall*
GOENKA, L.N.; PANTON, R.L.; BOGARD, D.G.*
Pressure and three-component velocity measurements in a diffuser that generates longitudinal vortices*
J. Fluids Engg. 112, 281*
1990. `
..06.0,59.0: square spanwise bars - k-type or d-type roughness*
LIOU, T.-M.; CHANG, Y.; HWANG, D.-W.*
Experimental and computational study of turbulent flows in a channel with two pairs of turbulence promoters in tandem*
J. Fluids Engg. 112, 302*
1990. `
..30.3: Grenoble - two test sections, including open channel*
BRIANCON-MARJOLLET, L.; MICHEL, J.M.*
The hydrodynamic tunnel of I.M.G. - former and recent equipments*
J. Fluids Engg. 112, 338*
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. `
..54.0: weakly nonlinear*
LEIBOVICH, S.*
Waves and bifurcations in vortex filaments*
Studies of Vortex Dominated Flows (M.Y. Hussaini and M.D. Salas, Eds.), p. 3*
1990. `
..54.0: linear instability - general review*
WIDNALL, S.E.*
Review of three-dimensional vortex dynamics - implications for the computation of separated and turbulent flows*
Studies of Vortex Dominated Flows (M.Y. Hussaini and M.D. Salas, Eds.), p. 16*
1990. `
..54.0: breakdown as a two-stage transition*
KELLER, J.J.; EGLI, W.; EXLEY, J.*
Force- and loss-free transitions between vortex flow states*
Studies of Vortex Dominated Flows (M.Y. Hussaini and M.D. Salas, Eds.), p. 63*
1990. `
..54.0: closed streamline solutions*
HAFEZ, M.M.; SALAS, M.D.*
Vortex breakdown simulation based on a nonlinear inviscid model*
Studies of Vortex Dominated Flows (M.Y. Hussaini and M.D. Salas, Eds.), p. 76*
1990. `
..27.2: latest review*
LE BALLEUR, J.C.*
Viscous-inviscid interaction solvers and computation of highly separated flows*
Studies of Vortex Dominated Flows (M.Y. Hussaini and M.D. Salas, Eds.), p. 159*
1990. `
..59.2,04.0: useful review from Notre Dame*
GAD-EL-HAK, M.*
Control of low-speed airfoil aerodynamics*
AIAA J. 28, 1537*
1990. `
..14.0: kinetic is the word - 3 families of eddies*
HONG, Z.-C.; LIN, C.*
Turbulent kinetic equations characterized by three and many nonequilibrium degrees of freedom*
AIAA J. 28, 1553*
1990. `
..24.1,48.0: inspired by Rockwell*
PANARAS, A.G.*
Shear-layer-edge interaction - simulation by finite-area vortices*
AIAA J. 28, 1557*
1990. `
..51.0,18.2: u-compt. HWA*
HYDE, C.R.; ET AL.*
Turbulence measurements for heated gas slot injection in supersonic flow*
AIAA J. 28, 1605*
1990. `
..13.0,18.1: Langley work - extended Johnson-King*
MITCHELTREE, R.A.; SALAS, M.D.; HASSAN, H.A.*
One-equation turbulence model for transonic airfoil flows*
AIAA J. 28, 1625*
1990. `
..29.6,32.2: good review - flow viz. plus gasdynamic properties*
HILLER, B.; HANSON, R.K.*
Properties of the iodine molecule relevant to laser-induced fluorescence experiments in gas flows*
Expts. in Fluids 10, 1*
1990. `
..48.0,62.0: Miller and Comings ride again (and see Lund AIAA J. 24, 1964, 1986 for static p., etc. in one-sided case)*
LIN, Y.F.; SHEU, M.J.*
Investigation of two plane parallel unventilated jets*
Expts. in Fluids 10, 17*
1990. `
..59.0,50.0: rotating cascade upstream*
PFEIL, H.; ORTH, U.*
Boundary-layer transition on a cylinder with and without separation bubbles*
Expts. in Fluids 10, 23*
1990. `
..23.0,44.1,06.0: absolute rms p fluctuation is a max. before trough - complicated spectrum evolution*
HANDLER, R.A.*
Turbulent wall pressure fluctuations over wavy surfaces*
Expts. in Fluids 10, 33*
1990. `
..29.6,32.2,11.6: just so*
VAN CRUYNINGEN, I.; LOZANO, A.; HANSON, R.K.*
Quantitative imaging of concentration by planar laser-induced fluorescence*
Expts. in Fluids 10, 41*
1990. `
..28.1,29.6: 2D correlation of digitized pictures*
BRAND, A.J.; HESSELINK, L.*
Auto-correlation measurements in three-dimensional fluid flow datasets*
Expts, in Fluids 10, 55*
1990. `
..31.1,05.0: finding inactive motion increasing with Re is a good test*
KLEWICKI, J.C.; FALCO, R.E.*
On accurately measuring statistics associated with small-scale structure in turbulent boundary layers using hot-wire probes*
J. Fluid Mech. 219, 119*
1990. `
..19.3: slope less than - 5/3 - modification of Gurvich and Yaglom 1967, using beta distribution*
YAMAZAKI, H.*
Breakage models - lognormality and intermittency*
J. Fluid Mech. 219, 181*
1990. `
..19.1: -1 . 300 -  literature review*
MOHAMED, M.S.; LaRUE, J.C.*
The decay power law in grid-generated turbulence*
J. Fluid Mech. 219, 195*
1990. `
..19.1: 450 x 450 mesh - automated vortex census*
McWILLIAMS, J.C.*
The vortices of two-dimensional turbulence*
J. Fluid Mech. 219, 361*
1990. `
..19.1: - see previous*
McWILLIAMS, J.C.*
The vortices of geostrophic turbulence*
J. Fluid Mech. 219, 387*
1990. `
..62.0: diametral jet in circular cylinder*
BREIDENTHAL, R.E.; BUONADONNA, V.R.; WEISBACH, M.F.*
Molecular mixing via jets in confined volumes*
J. Fluid Mech. 219, 531*
1990. `
..24.2: inviscid*
GOLDSTEIN, M.E.; WUNDROW, D.W.*
Spatial evolution of nonlinear acoustic mode instabilities on hypersonic boundary layers*
J. Fluid Mech. 219, 585*
1990. `
..18.1: just so*
COAKLEY, T.J.; VIEGAS, J.R.; HUANG, P.G.; RUBESIN, M.W.*
An assessment and application of turbulence models for hypersonic flows*
Presented at 9th Nat. Aero-Space Plane Tech. Sympo., paper no. 106*
1990. `
..43.1: discussion of eddy viscosity and intermittency*
PLEUNE, R.*
Vertical diffusion in the stable atmosphere*
Atmos. Env. 24A, 2547*
1990. `
..44.2: review and suggestions for future research--JPJ has*
GRAHAM, R.W.*
Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine*
ASME 90-GT-100*
1990. `
..44.2: migrate to pressure side---see also Harasgama, ASME GT-90-174*
KROUTHEN, B.; GILES, M.B.*
Numerical investigation of hot streaks in turbines*
J Prop. Power 6, 769*
1990. `
..44.2: hot gas transported to pressure side - mainly in endwall boundary layer. NS and STAN5 calcs.*
HARASGAMA, S.P.*
Combustor exit temperature distortion effects on heat transfer and aerodynamics within a rotating turbine blade passage.*
ASME paper 90-GT-174*
1990. `
..44.2: calculations - JPJ has*
METZGER, D.E.; DUNN, M.G.; HAH, C.*
Turbine tip and shroud heat transfer*
ASME 90-GT-333*
1990. `
..60.0: chooses 12 out of 105 references*
SETTLES, G. S.; DODSON, L. J.*
Hypersonic shock/boundary-layer interaction database*
Penn State University Report PSU-ME-90/91-003*
1990. `
..11.6,02.1: flame surface dimension 2.28---lower than for non-reacting flows*
TAKENO, T.; MURAYAMA, M.; TANIDA, Y.*
Fractal analysis of turbulent premixed flame surface*
Expts. in Fluids 10, 61*
1990. `
..29.6: iso-concentration surfaces of smoke scanned with traversing laser sheet*
YODA, M.; HESSELINK, L.*
A three-dimensional visualization technique applied to flow around a delta wing*
Expts. in Fluids 10, 102*
1990. `
..24.1,29.16: including 5 cm dia circular smoke wire*
KUSEK, S. M.; CORKE, T. C.; REISENTHEL, P.*
Seeding of helical modes in the initial region of an axisymmetric jet*
Expts. in Fluids 10, 116*
1990. `
..32.1: 30 or 50 mW Hitachi laser diodes---drifts in calibration of LDV due to thermal expansion etc.*
DURST, F.; MULLER, R.; NAQWI, A.*
Measurement accuracy of semiconductor LDA systems*
Expts. in Fluids 10, 125*
1990. `
..32.2: calibrate by automatic tracking of synthetic images*
GUEZENNEC, Y. G.; KIRITSIS, N.*
Statistical investigation of errors in particle image velocimetry*
Expts. in Fluids 10, 138*
1990. `
..24.1,18.2: seem to agree better with Bogdan than Roshko*
SCHADOW, K. C.; GUTMARK, E.; WILSON, K. J.*
Compressible spreading rates of supersonic coaxial jets*
Expts. in Fluids 10, 161*
1990. `
..11.3,29.6: rhodamine B. LIF and photomultiplier to measure intensity*
ARCOUMANIS, C.; McGUIRK, J.J.; PALMA, J.M.L.M.*
On the use of fluorescent dyes for concentration measurements in water flows*
Expts. in Fluids 10, 177*
1990. `
..54.0,19.1: 30 cm, 20 m/s, 800 rpm see also TSF 6*
JACQUIN, L.; LEUCHTER, O.; CAMBON, C.; MATHIEU, J.*
Homogeneous turbulence in the presence of rotation*
J. Fluid Mech. 220, 1*
1990. `
..24.5,25.5: bubble, with vortex shedding from separation, at shear-layer instability frequency*
PAULEY, L.P.; MOIN, P.; REYNOLDS, W.C.*
The structure of two-dimensional separation*
J. Fluid Mech. 220, 397*
1990. `
..24.2,24.4: see also MIT FDRL 88-11 and p. 595. Advective part initially stronger but decays leaving only the travelling wave part*
BREUER, K.S.; HARITONIDIS, J.H.*
The evolution of a localized disturbance in a laminar boundary layer. Part 1. Weak disturbances*
J. Fluid Mech. 220, 569*
1990. `
..24.2,24.4: low-speed streak boundary by shear layers---x,y plane layer has secondary instability.  See also p.569*
BREUER, K.S.; LANDAHL, M.T.*
The evolution of a localized disturbance in a laminar boundary layer. Part 2.  Strong disturbances.*
J. Fluid Mech. 220, 595*
1990. `
..24.2,53.0: extension and correction of JFM 204, 405 by P. Hall and Seddoughi - now many neutral modes*
BASSOM, A.P.; SEDDOUGUI, S.O.*
The onset of three-dimensionality and time-dependence in Gortler vortices - neutrally stable wavy modes*
J. Fluid Mech. 220, 661*
1990. `
..06.0,59.0,61.0: 2D and 3D rectangular blocks---on inner layer scales*
SCHOFIELD, W.H.; LOGAN, E.*
Turbulent shear flow over surface mounted obstacles*
J. Fluids Engg 112, 376*
1990. `
..59.0,61.0: four regions of St vs. Re - St range 0.16 to 0.24*
SAKAMOTO, H; HANIU, H.*
A study on vortex shedding from spheres in a uniform flow*
J. Fluids Engg 112, 386*
1990. `
..45.0,61.0: one with straight-tapered trailing edge--horseshoe vortex detectable only with this one, large swirls with common flow up in both cases.  See p. 441*
EIBECK, P.A.*
An experimental study of the flow downstream of a circular and tapered cylinder*
J. Fluids Engg 112, 393*
1990. `
..59.0,23.0: simplistic use of probe-microphone static tube within flow*
GOVINDA RAM, H.S.; ARAKERI, V.H.*
Studies on unsteady pressure fields in the region of separating and reattaching flows*
J. Fluids Engg 112, 402*
1990. `
..45.0,16.2: radial and axial intensities only - no shear stresses at all*
IACOVIDES, H.; LAUNDER, B.E.; LOIZOU, P.A.; ZHAO, H.H.*
Turbulent boundary-layer development around a square-sectioned U-bend -  measurements and computation*
J. Fluids Engg 112, 409*
1990. `
..05.0,07.0: matched asymptotic matching parameter, equal to friction velocity only at infinite Reynolds number*
PANTON, R.L.*
Scaling turbulent wall layers*
J. Fluids Engg 112, 425*
1990. `
..45.0,61.0: cylinder with straight-tapered trailing edge--skin friction increased downstream.  See p. 393.*
PIERCE, F.J.; NATH, S.K.*
Interference drag of a turbulent junction vortex *
J. Fluids Engg 112, 441*
1990. `
..51.0,61.0: mean horseshoe vortices in near field--they discuss ensemble-average fluctuation too.*
MATSUDA, H.; IIDA, S.-I.; HAYAKAWA, M.*
Coherent structures in a three-dimensional wall jet*
J. Fluids Engg 112, 462*
1990. `
..14.0,05.1: nonlinear quadratic terms in Reynolds stress as such (not in eddy viscosity)*
MYONG, H.K.; KASAGI, N.*
Prediction of anisotropy of the near-wall turbulence with an anisotropic low-Reynolds-number k, eps. turbulence model*
J. Fluids Engg 112, 521*
1990. `
..11.3,28.2: must base on adiabatic temperature, not mean fluid temperature*
MOFFAT, R.J.; ANDERSON, A.M.*
Applying heat transfer coefficient data to electronics cooling*
J. Heat Transfer 112, 882*
1990. `
..14.0,10.0,42.1: k, eps. and ASM with T closures - ASM no better, and all drastically underpredict axial heat transfer*
SHABBIR, A.; TAULBEE, D.B.*
Evaluation of turbulence models for predicting buoyant flows*
J. Heat Transfer 112, 945*
1990. `
..25.2,59.2: general discussion of code validation*
MEHTA, U.B.*
The aerospace plane design challenge - credible computational fluid dynamics results*
NASA TM 102887*
1990. `
..06.0,22.1,30.1: log-law modifications - relevant to wind tunnel acoustic treatment*
FLYNN, K.P.; PANTON, R.L.; BOGARD, D.G.*
Effect of Helmholtz resonators on boundary-layer turbulence*
AIAA J. 28, 1857*
1990. `
..14.0,44.2: ASM better than k, eps.*
ZHANG, J.; LAKSHMINARAYANA, B.*
Computation and turbulence modeling for three-dimensional boundary layers including turbomachinery rotary flows*
AIAA J. 28, 1861*
1990. `
..09.3,05.0: suggests outer layer structures not essential to wall-layer process*
WARK, C.E.; NAGUIB, A.M.; NAGIB, H.M.*
Effect of plate manipulators on coherent structures in a turbulent boundary layer*
AIAA J. 28, 1877*
1990. `
..50.0,03.0: rotating rod generator - BL relaminarization after wake passes*
RENOUD, R.W.; HOWARD, R.M.*
Airfoil boundary-layer response to an unsteady turbulent flow field*
AIAA J. 28, 1894*
1990. `
..18.1,15.0: reproduces Langley curve - physics not clear*
KIM, S.C.*
New mixing-length model for supersonic shear layers*
AIAA J. 28, 1999*
1990. `
..13.0,18.1: Johnson-King upgrade -- slightly dubious mixed velocity scale for inner layer*
JOHNSON, D.A.; COAKLEY, T.J.*
Improvements to a nonequilibrium algebraic turbulence model*
AIAA J. 28, 2000*
1990. `
..31.2: high Re of wedge probes reduces M effect - refers to Dewey who said it was really Kn effect*
DEMETRIADES, A.; ANDERS, S.G.*
Characteristics of hot-film anemometers for use in hypersonic flows*
AIAA J. 28, 2003*
1990. `
..45.0,61.0: does not prevent leading-edge separation or bistable unsteadiness -  was 89-0986*
DEVENPORT, W.J.; ET AL.*
Effects of a fillet on the flow past a wing-body junction*
AIAA J. 28, 2017*
1990. `
..24.1: published version of 90-0505*
BELL, J.H.; MEHTA, R.D.*
Development of a two-stream mixing layer from tripped and untripped boundary layers*
AIAA J. 28, 2034*
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. `
..25.7: just so - exact to linear approximation*
GILES, M.B.*
Nonreflecting boundary conditions for Euler equation calculations*
AIAA J. 28, 2050*
1990. `
..25.6: DNS results show typically 50 percent of LES points experience backscatter*
PIOMELLI, U.; CABOT, W.H.; MOIN, P.; LEE, S.*
Subgrid-scale backscatter in transitional and turbulent flow*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 19*
1990. `
..25.6,18.1: development of new Metais and Lesieur model*
COMTE, P.; LEE, S.; CABOT, W.H.*
A subgrid-scale model based on the second-order velocity structure function*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 31*
1990. `
..25.6: generalization of Smago., plus parameterization of shocklet dissipation*
SQUIRES, K.; ZEMAN, O.*
On the subgrid-scale modeling of compressible turbulence*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 47*
1990. `
..13.0,18.1: "transport" equation for pressure-dilatation product*
AUPOIX, B.; BLAISDELL, G.A.; REYNOLDS, W.C.; ZEMAN, O.*
Modeling the turbulent kinetic energy equation for compressible, homogeneous turbulence*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 63*
1990. `
..13.0,16.1,05.0: mainly duct with z-wise p.g., plus preview of Pontikos*
BRADSHAW, P.; SENDSTAD, O.*
Structure of three-dimensional turbulent boundary layers*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 75*
1990. `
..14.0: c_mu and near-wall damping function f_mu, plus improved dissipation equation*
RODI, W.; MANSOUR, N.N.*
Low Reynolds number k, eps. modeling with the aid of direct simulation data*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 85*
1990. `
..14.0: evaluation of length scales, plus use of v intensity instead of TKE (needs no damping)*
RODI, W.; MANSOUR, N.N.*
One-equation near-wall turbulence modeling with the aid of direct simulation data*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 107*
1990. `
..11.1,05.0: significant differences between heat and mom. transport, due to pressure.  Why was Reynolds right? Undermines flow viz.*
GUEZENNEC, Y.; STRETCH, D.; KIM, J.*
The structure of turbulent channel flow with passive scalar transport*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 127*
1990. `
..11.1: see G, S and K*
STRETCH, D.; GUEZENNEC, Y.; KIM, J.*
Heat and momentum exchange mechanism in turbulent channel flow*
 Bull. Am. Phys. Soc. 35, 2304*
1990. `
..24.1,18.1,19.2: possibly first reference to oblique disturbances at M_c=0.8 - but no direct relation to the "pasta problem" of high-k geometry*
CHEN, J.H.; ET AL.*
A study of the topology of dissipating motions in direct numerical simulations of time-developing compressible and incompressible mixing layers*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 139*
1990. `
..42.1: see Gibson - agrees with lab expt.*
ITSWEIRE, E.C.; HOLT, S.E.; KOSEFF, J.R.; FERZIGER, J.H.*
Direct numerical simulations of stably-stratified sheared turbulence - implications for oceanic mixing*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 163*
1990. `
..11.2,19.2: Batchelor scaling works at low Re - at high Re the small-scale strain rate is irrelevant*
GIBSON, C.; ROGERS, M.; CHASNOV, J.; PETRESKY, J.*
Numerical simulation of low Prandtl number turbulent mixing*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 211*
1990. `
..24.1,02.1: peak-valley counting (pvc) technique - enstrophy much more intermittent than dissipation*
ZOHAR, Y.; MOSER, R.D.; BUELL, J.C.; HO, C.M.*
Length scales and dissipation of fine eddies in a mixing layer*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 225*
1990. `
..24.1,11.6,01.1: transition from dimension 4/3 to 5/3 in first pairing *
JIMENEZ, J.; MARTEL, C.*
A fractal transition in the two dimensional shear layer*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 235*
1990. `
..11.6: triangular Z-Y diagrams*
MELL, W.E.; KOSALY, G.; PLANCHE, O.; POINSOT, T.; FERZIGER, J.H.*
Laminar flamelet modeling of turbulent diffusion flames*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 255*
1990. `
..11.6,01.2: flame front wrinkles more for Le less than 1*
RUTLAND, C.J.; TROUVE, A.*
Pre-mixed flame simulations for non-unity Lewis numbers*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 299*
1990. `
..42.3: finite density variations, but no velocity, at t=0*
CHASNOV, J.R.; ROGALLO, R.S.*
Generation of large-scale density fluctuations by buoyancy*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 313*
1990. `
..19.2: highly intermittent local transfer resulting from non-local interaction*
DOMARADZKI, J.A.; ROGALLO, R.S.; WRAY, A.A.*
Interscale energy transfer in numerically simulated homogeneous turbulence*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 319*
1990. `
..19.2,02.1,28.1: defines a scale-dependent high frequency intermittency and a spatially-local Reynolds number*
FARGE, M.; GUEZENNEC, Y.; HO. C.M.; MENEVEAU, C.*
Continuous wavelet analysis of coherent structures*
Studying Turbulence Using Numerical Simulation Databases III (NASA Ames/Stanford Center for Turbulence Research), p. 331*
1990. `
..25.10: knowledge-based approach*
VOGEL, A.A.*
Automated domain decomposition for computational fluid dynamics*
Computers and Fluids 18, 329*
1990. `
..25.10: non-orthogonal coordinates*
CEBECI, T.; CHEN, H.H.; KAUPS, K.*
A method for removing the coordinate singularity on bodies with blunt rounded noses at incidence*
Computers and Fluids 18, 369*
1990. `
..22.2: including turbulence, vortex breakdown etc  --fascinating/hilarious. Authors are editors.*
TREFETHEN, L.M.; PANTON, R.L.*
Some unanswered questions in fluid mechanics*
Appl. Mech. Rev. 43, 153*
1990. `
..28.1:Version 3 . 6 b+*
WALATKA, P.P.; BUNING, P.G.; PIERCE, L.; ELSON, P.A.*
PLOT3D user's manual*
NASA TM 101067*
1990. `
..25.6:  Smago. SGS - see 90-01 for a pure finite difference code*
MADABHUSHI, R.K.; VANKA, S.P.*
Large eddy simulation of channel flow using a mixed spectral finite difference technique*
U. of Illinois at Urbana-Champaign, Rept. No. CFD 90-08*
1990. `
..11.1,19.2:  alternative to lognormal, for vel. or temp.*
ANDREWS, L.C.; SHIVAMOGGI, B.K.*
The gamma distribution as a model for temperature dissipation in intermittent turbulence*
Phys. Fluids A2, 105*
1990. `
..24.2:  also recent JFM? Increases growth rate of T-S and the 3D sub.*
NAYFEH, A.H.; RAGAB, S.A.; MASAD, J.A.*
Effect of a bulge on the subharmonic instability of boundary layers*
Phys. Fluids A2, 937*
1990. `
..24.2,50.0:  unsteadiness in free stream causes instability even on a linear analysis*
THOMPSON, C.; MANLEY, M.G.*
Linear stability of stagnation flow*
Phys. Fluids A2, 1350*
1990. `
..24.1,11.6:  just so*
ROSHKO, A.*
The mixing transition in free shear flows*
NATO Workshop on the Global Geometry of Turbulence (Cadiz)*
1990. `
..28.1,29.6:  PLOT 3D etc.*
WATSON, V.; WALATKA, P.P.; BANCROFT, G.; PLESSEL, T.; MERRITT, F.*
Visualization of fluid dynamics at NASA Ames*
Computing Systems in Engg. 1, 333*
1990. `
..31.1,25.6: X-probe spacing of 3 plus-units gives rms v 50 percent high at y^+ = 10 - presumably du/dz effect. JKE has Proc.*
SUZUKI, Y.; KASAGI, N.*
Evaluation of hot-wire measurements in turbulent wall shear flows using a DNS data base*
Engineering Turbulence Modelling and Experiments (Rodi and Ganic, eds.), Elsevier, p. 361*
1990. `
..14.0:  2-equation models*
CEBECI, T.*
Turbulence modelling requirements of aerodynamic flows*
Engineering Turbulence Modelling and Experiments (Rodi and Ganic, eds.), Elsevier, p. 499*
1990. `
..31.1,32.2:  LIF for p. fluctuations - see Gross 1985, 1987 for details.  Total T fluctuations not negligible.*
LOGAN, P.; McKENZIE, R.L.; BERSHADER, D.*
Accuracy of hot-wire measurements in supersonic turbulence from comparisons with laser-induced fluorescence*
NASA Tech Brief ARC-12104*
1990. `
..54.0:  only for a nonslip wall*
ORLANDI, P.*
Vortex dipole rebound from a wall*
Phys. Fluids A2, 1429*
1990. `
..54.0:  inviscid but nonlinear*
TYVAND, P.A.*
On the interaction between a strong vortex pair and a free surface*
Phys. Fluids A2, 1624*
1990. `
..13.0:  traditional equation correct only for isotropy - and agrees with RDT*
KASSINOS, S.C.; REYNOLDS, W.C.*
Tensorial volume of turbulence revisited*
Phys. Fluids A2, 1669*
1990. `
..13.0,54.0:  second-order closures better than two-equation models*
SPEZIALE, C.G.; GATSKI, T.B.; Mac GIOLLA MHUIRIS, N.*
A critical comparison of turbulence models for homogeneous shear flows in a rotating frame*
Phys. Fluids A2, 1678*
1990. `
..14.0:  third-order anisotropy in k, eps.*
HORIUTI, K.*
Higher-order terms in the anisotropic representation of Reynolds stresses*
Phys. Fluids A2, 1708*
1990. `
..05.0:  mean shear is what counts - as witness air flow over the liquid*
RASHIDI, M.; BANERJEE, S.*
The effect of boundary conditions and shear rate on streak formation and breakdown in turbulent channel flows*
Phys. Fluids A2, 1827*
1990. `
..13.0:  relating anisotropy of dissipation to that of Reynolds stress*
HALLBACK, M.; GROTH, J.; JOHANSSON, A.V.*
An algebraic model for nonisotropic turbulent dissipation rate in Reynolds stress closures*
Phys. Fluids A2, 1859*
1990. `
..11.1:  oddities at infinite Sc*
DIMOTAKIS, P.E.; MILLER, P.L.*
Some consequences of the boundedness of scalar fluctuations*
Phys. Fluids A2, 1919*
1990. `
..12.2:  second-order system - relevance to Burgulence unclear*
BHAT, G.S., NARASIMHA, R.; WIGGINS, S.*
A simple dynamical system that mimics open-flow turbulence*
Phys. Fluids A2, 1983*
1990. `
..24.1,54.0:  vortex decays rapidly, and uw rises to 40 percent of uv*
BELL, J.H.; MEHTA, R.D.*
Interaction of a streamwise vortex with a turbulent mixing layer*
Phys. Fluids A2, 2011*
1990. `
..24.4:  Re of 1600 based on half-width and max. vel. - loudspeaker*
KLINGMANN, B.G.B.; ALFREDSSON, P.H.*
Turbulent spots in plane Poiseuille flow -- measurements of the velocity field*
Phys. Fluids A2, 2183*
1990. `
..01.1,05.0:  proper orthogonal decomposition - wave speed is flow speed at position of max. Reynolds stress*
SIROVICH, L.; BALL, K.S., KEEFE, L.R.*
Plane waves and structures in turbulent channel flow*
Phys. Fluids A2, 2217*
1990. `
..24.1,01.1:  first pairing region of mixing layer - 4 modes are enough*
RAJAEE, M.; KARLSSON, S.K.F.*
Shear flow coherent structures via Karhunen-Loeve expansion*
Phys. Fluids A2, 2249*
1990. `
..08.0,59.2:  Boeing work - so shelved*
ANON.*
Application of laminar flow control to supersonic transport configurations*
NASA Contractor Report 181917*
1990. `
..28.1,29.6:  PLOT 3D etc.*
WATSON, V.; WALATKA, P.P.; BANACROFT, G.; PLESSEL, T.; MERRITT, F.*
Visualization of fluid dynamics at NASA Ames*
Computing Systems in Engg. 1, 333*
1990. `
..09.3:  implies necessity for vortex street, easier at low Re*
BERTELRUD, A.; LIANDRAT, M.-P.*
Large eddy breakup devices at low and high Reynolds numbers*
AIAA 90-1601*
1990. `
..24.4:  spreading rate reduced, and ratio of leading to trailing edge propagation velocity less than for flat plate*
KATZ, Y.; SEIFERT, A.; WYGNANSKI, I.*
On the evolution of the turbulent spot in a laminar boundary layer with a favourable pressure gradient*
J. Fluid Mech. 221, 1*
1990. `
..17.1:  frequencies up to burst freq., but still quasi-steady*
BRERETON, G.J.; REYNOLDS, W.C.; JAYARAMAN, R.*
Response of a turbulent boundary layer to sinusoidal free-stream unsteadiness*
J. Fluid Mech. 221, 131*
1990. `
..24.2:  spatial stability - yes, full N-S*
FASEL, H.; KONZELMANN, U.*
Non-parallel stability of a flat-plate boundary layer using the complete Navier-Stokes equations*
J. Fluid Mech. 221, 311*
1990. `
..54.0:  published version - calcs. for cylinder with rotating base.  Breakdown seems to be equated with recirculation.  See p. 553.*
LOPEZ, J.M.*
Axisymmetric vortex breakdown.  Part 1.  Confined swirling flow*
J. Fluid Mech. 221, 533*
1990. `
..54.0:  see p. 533 - production of a negative azimuthal (circumferential) component.  "The relatively sudden appearance of a rapid divergence in the stream surfaces, and the corresponding appearance of recirculation zones.."*
BROWN, G.L.; LOPEZ, J.M.*
Axisymmetric vortex breakdown.  Part 2.  Physical mechanisms*
J. Fluid Mech. 221, 553*
1990. `
..13.0:  discussion of velocity/pressure-gradient correlation - more relevant than pressure-strain*
LAI, Y.G.; SO, R.M.C.*
On near-wall turbulent flow modelling*
J. Fluid Mech. 221, 641*
1990. `
..25.2:  philosophical/AI discussion, including Plato*
NAKAMURA, I.; WATANABE, T.*
Fundamental study of the problem solver for fluids engineering*
Memoirs Faculty of Engg., Nagoya Univ., 42, 183*
1990.`
..54.0,45.0,61.0:  vorticity attenuates much faster than in 2D - but is it the bending of the vortex, or the crossflow as such?*
SHIZAWA, T.; EATON, J.K.*
Interaction of an embedded longitudinal vortex with an attached, three-dimensional, turbulent boundary layer*
Stanford University Mech. Engg Report MD-56*
1990.`
..59.2,54.2:  detailed review*
LEE, M.; HO, C.-M.*
Lift force of delta wings*
Appl. Mech. Rev. 43, 209*
1990.`
..53.0,50.0:  neologism is just "independence of history" - up to 8 percent turbulence behind crossbar*
HEINIGER, K.C.*
Investigation of the "energy stratification" in turbulent flow in a curved duct, Vols. I and II*
Ph.D. Thesis, ETH Zurich, No. 9344*
1990. `
..19.2,53.0:  decay rate decreases as a result of production*
JOHNSON, P.L.; JOHNSTON, J.P.*
The effect of streamline curvature on decaying grid turbulence*
Twelfth Symposium on Turbulence, Rolla*
1990. `
..13.0:  linearized pertubation analysis*
GAO, G.; CHOW, W.L.*
A new theory of turbulence based on the concept of fractal analysis*
ICAS paper 90-6.10R2*
1990. `
..01.1,24.1:  general review*
WALLACE, J.M.; HUSSAIN, F.*
Coherent structures in turbulent shear flows*
Appl. Mech. Rev. 43, S203*
1990. `
..25.5:  general curvi. coords.*
JOSHI, D.S.; VANKA, S.P.*
A multigrid calculation procedure for internal flows in complex geometries*
AIAA-90-0442*
1990. `
..11.2: liquid crystals and image processing - review*
MOFFAT, R.J.*
Experimental heat transfer*
Proc. 9th Int. Heat Transf. Conf., Jerusalem (G. Hetsroni, ed.), vol. 1, p. 187*
1991. `
..13.0,14.0,18.1:  emphasis on compressible flow - 5 - pages, 10 figs.*
MARVIN, J.G.*
Progress and challenges in modeling turbulent aerodynamic flows*
Presented at Engineering Turbulence Modelling Conference, Dubrovnik*
1990. `
..11.6:  general review plus simple explanation of p.d.f. method*
POPE, S.B.*
Computations of turbulent combustion - progress and challenges*
Twenty-third Symposium (International) on Combustion/The Combustion Institute, p. 591*
1990. `
..16.1,13.0,14.0: simple models, up to Johnson-King*
BETTELINI, M.S.G.*
Numerical study of some engineering turbulence models for three-dimensional boundary layers*
Diss. ETH No. 9182*
1990. `
..09.5,24.1,50.0: well-laid-out chronicle*
FIEDLER, H.E.; FERNHOLZ, H.-H.*
On management and control of turbulent shear flows*
Prog. Aerospace Sci. 27, 305*
1990. `
..12.2: small perturbations - reminiscent of psychohistory*
OTT, E.; GREBOGI, C.; YORKE, J.A.*
Controlling Chaos*
Phys. Rev. Letters 66, 1196*
1990. `
..13.0,14.0,59.0: review*
FERZIGER, J.H.*
Approaches to turbulent flow computation - applications to flow over obstacles*
J. Wind Eng. and Indust. Aero. 35, 1*
1990. `
..25.5,44.2: Poisson for pressure - novelty not apparent*
FERRAND, P.; LEBOEUF, F.; POMMEL, F.; PARKINSON, E.*
Parabolized calculations of turbulent three dimensional flows in a turbine duct*
AGARD-CP-469, "Secondary flows in turbomachines" paper 4*
1990. `
..62.0: k,eps. calcs - intake and nozzles*
TAFTI, D.; VANKA, S.P.*
Hot gas environment around STOVL aircraft in ground proximity. Part II - Numerical study*
AIAA-90-2270*
1990. `
..50.0,44.2: cylindrical spokes*
SCHULZ, H.D.; GALLUS, H.E.*
Experimental investigation of the influence of rotor wakes on the development of the profile boundary layer and the performance of an annular compressor cascade*
AGARD-CP-468*
1990. `
..23.0: 121-microphone array - approximation to k_1, k_3 spectra*
SHERMAN, C.H.; KO, S.H.; BUEHLER, B.G.*
Measurement of the turbulent boundary layer wave-vector spectrum*
J. Acoust. Soc. Am. 86, 386*
1990. `
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