Shock Tube Application to the Study of Compressible Turbulent Boundary Layer with Mass Injection

Author:

Liaw J.-Y.,Bershader D.

Publisher

Springer Berlin Heidelberg

Reference13 articles.

1. Bershader D, Allport J (1956) On the laminar boundary layer induced by a traveling shock wave. NR061–020, Department of Physics, Princeton University

2. Davies DR, Berstein L (1969) Heat transfer and transition to turbulence in the shock-induced boundary layer on a semi-infinite flat plate, Part 1. J. Fluid Mechs. 36: 87–112

3. Fitt AD, Ockendon JR, Jones TV (1985) Aerodynamics of slot film cooling: theory and experiment. J. Fluid Dynamics 160: 15–27

4. Forth CJP, Jones TV (1986) Scaling parameters in film-cooling. In: Tien CL, Carey VP, Ferrell JK (eds) Heat Transfer, Vol. 3, pp 1271–1276

5. Gladden HJ, Yeh FC, Austin PJ Jr.(1987) Computation of full-cover age film-cooled airfoil temperature by two methods and comparison with high heat flux data. ASME-GT-213, Gas Turbine Conference and Exhibition, Anaheim, California, May 31 – June 4

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