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Documentation of Experimental Data for Hypersonic 3-D Shock Waves
Schülein, E. and Zheltovodov, A.A. (2001) Documentation of Experimental Data for Hypersonic 3-D Shock Waves. DLR-Interner Bericht. 99 A 26, 95 S.
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Abstract
Experimental data for a series of three-dimensional hypersonic swept- and crossing-shock-waves / turbulent boundary layer interaction flows in the vicinity of one and two sharp fins mounted on a flat plate are presented. The data contains detailed documentation of incoming boundary layer, surface pressure and heat flux distributions, skin friction distributions and topological features of the limiting streamlines in the interaction region at M = 5. The deflection angles ß were varied for swept-shock interactions (single fin geometry) from 0° to 27°, and for crossing-shock interaction (double fin geometry) from 8° to 23°.
| Document Type: | Monograph (DLR-Interner Bericht) | ||||||
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| Additional Information: | LIDO-Berichtsjahr=2001, | ||||||
| Title: | Documentation of Experimental Data for Hypersonic 3-D Shock Waves | ||||||
| Authors: |
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| Date: | 2001 | ||||||
| Number of Pages: | 95 | ||||||
| Status: | Published | ||||||
| Keywords: | hypersonic flow, swept shock, crossing shock, turbulent boundary layer, | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | L - no assignement | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | L ST - Starrflüglertechnologien | ||||||
| DLR - Research theme (Project): | L - Military Technologies | ||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology | ||||||
| Deposited By: | elib DLR-Beauftragter | ||||||
| Deposited On: | 31 Jan 2006 | ||||||
| Last Modified: | 14 Jan 2010 18:49 |
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