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Documentation of Two- and Three-Dimensional Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows (1989)

Kussoy, Marvin I. ; Horstman, Clifford C.

In: CASI

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Publication Date: 2019-06-28

Description: Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer interaction flows at Mach 7 are presented. Test bodies, composed of simple geometric shapes, were designed to generate flows with varying degrees of pressure gradient, boundary-layer separation, and turning angle. The data include surface-pressure and heat-transfer distributions as well as limited mean-flow-field surveys in both the undisturbed and the interaction regimes. The data are presented in a convenient form for use in validating existing or future computational models of these generic hypersonic flows.

Keywords: AERODYNAMICS

Type: NASA-TM-101075 , A-89048 , NAS 1.15:101075

Format: application/pdf

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