Subsonic impulsively starting flow at a high angle of attack with shock wave and vortex interaction
Chinese journal of aeronautics ; 31 , 9 ; 1822-1828
01.01.2018
7 pages
Aufsatz (Zeitschrift)
Englisch
DDC: | 629.13005 |
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High angle-of-attack calculations of the subsonic vortex flow on slender bodies
Tema Archiv | 1985
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