Investigation of the shock wave/boundary layer interaction of scramjet intake flows
2010
XVI, 178 S.
21 cm
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Theses
English
BKL: | 50.34 Gasdynamik, Aerodynamik / 50.03 Methoden und Techniken der Ingenieurwissenschaften / 55.50 Luftfahrzeugtechnik | |
RVK: | ZO 8150 | |
DDC: | 629.1343535 |
Investigation of the shock wave/boundary layer interaction of scramjet intake flows
Tema Archive | 2010
|Shock-Wave-Boundary-Layer Interactions in a Model Scramjet Intake
Online Contents | 2009
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