The Hypersonic Shock Wave Turbulent Boundary Layer Interaction Generated By A Sharp Fin At Mach 82
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Documentation of Two- and Three-dimensional Hypersonic Shock Wave/turbulent Boundary Layer Interaction Flows
Author | : Marvin I. Kussoy |
Publisher | : |
Total Pages | : 32 |
Release | : 1989 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Intersecting Shock-Wave/Turbulent Boundary-Layer Interactions at Mach 8. 3
Author | : National Aeronautics and Space Adm Nasa |
Publisher | : |
Total Pages | : 54 |
Release | : 2018-10-28 |
Genre | : |
ISBN | : 9781729362488 |
Experimental data for two three-dimensional intersecting shock-wave/turbulent boundary-layer interaction flows at Mach 8.3 are presented. The test bodies, composed of two sharp fins fastened to a flat-plate test bed, 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 mean flow-field surveys both in the undisturbed and interaction regimes. The data are presented in a convenient form to be used to validate existing or future computational models of these hypersonic flows. The data are also on a 3.5-inch diskette included and are available through E-mail. Kussoy, M. I. and Horstman, K. C. Ames Research Center...
Shock Wave - Turbulent Boundary Layer Interaction in High Speed Flow
Author | : Michael S. Holden |
Publisher | : |
Total Pages | : 188 |
Release | : 1975 |
Genre | : Aerodynamic heating |
ISBN | : |
Documentation of Two- And Three-Dimensional Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 28 |
Release | : 2018-07-02 |
Genre | : |
ISBN | : 9781722182298 |
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. Kussoy, Marvin I. and Horstman, Clifford C. Ames Research Center NCC2-452; RTOP 505-80-11...