Effect of shock impingement on heat transfer

Report (1973)
Copyright: © 1973 Von Karman Institute for Fluid Dynamics
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Published Date

01-05-1973

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VKI Training Center for Experimental Aerodynamics Technical Note 87

Abstract

The static pressure and heat transfer rate distributions have been measured in the reattachment region of free shear layers. In the first part, a cone/cavity model and the effects of gas injection have been studied. Results have been presented for both laminar and turbulent flows. In the second part, a flow model has been investigated which is analogous with an Edney type III shockwave interaction, found when the bow shock of a blunt hypersomic body is intersected by an extraneous shock.