论文信息 - Thin-layer approximation and algebraic model for separated turbulent flows - 字舞流文

Thin-layer approximation and algebraic model for separated turbulent flows

H. Lomax | B. Baldwin

[1] Gary S. Settles,et al. Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner , 1976 .

[2] W. L. Hankey,et al. Numerical Solution for Supersonic Turbulent Flow over a Compression Ramp , 1975 .

[3] R. Maccormack,et al. A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactions , 1975 .

[4] B. Baldwin,et al. Calculation of shock-separated turbulent boundary layers , 1975 .

[5] D. C. Reda,et al. Shock wave-turbulent boundary layer interactions in rectangular channels. II - The influence of sidewall boundary layers on incipient separation and scale of the interaction. , 1973 .

[6] Tuncer Cebec,et al. Calculation of Compressible Turbulent Boundary Layers with Heat and Mass Transfer , 1971 .

[7] E. Hopkins,et al. An evaluation of theories for predicting turbulent skin friction and heat transfer on flat plates at supersonic and hypersonic Mach numbers , 1971 .