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[American Institute of Aeronautics and Astronautics 27th Aerospace Sciences Meeting - Reno,NV,U.S.A. (09 January 1989 - 12 January 1989)] 27th Aerospace Sciences Meeting - Mach number dependence of flow separation induced by normal shock-wave/turbulent boundary-layer interaction at a curved wall

โœ Scribed by DOERFFER, P.; DALLMANN, U.


Book ID
121035911
Publisher
American Institute of Aeronautics and Astronautics
Year
1989
Weight
689 KB
Category
Article

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