Hypersonic turbulent boundary layer in adverse pressure gradients studied for transition, measuring static/pitot pressure, stagnation temperature and heat transfer rates
An experimental investigation of hypersonic turbulent boundary layers in adverse pressure gradient.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING ; 1968 ; NEW YORK, NY
1969-01-01
Miscellaneous
No indication
English
Empirical Modeling of Pressure Spectra in Adverse Pressure Gradient Turbulent Boundary Layers
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