A good knowledge of the turbulence structure, wall heat transfer, and friction in turbulent boundary layers (TBL) at high speeds is required for the design of hypersonic air breathing airplanes and reentry space vehicles. This work reports on recent progress in the modeling of high speed TBL flows. The specific research goal described here is the development of a second order closure model for zero pressure gradient TBL's for the range of Mach numbers up to hypersonic speeds with arbitrary wall cooling requirements.
Progress in modeling hypersonic turbulent boundary layers
1993-01-01
Miscellaneous
No indication
English
Reduced-Order Modeling of Hypersonic Turbulent Boundary Layers
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