Twin tail/delta wing configuration buffet due to unsteady vortex breakdown flow
14th Applied Aerodynamics Conference ; 1996 ; New Orleans , LA , U.S.A.
1996-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
VORTEX CONTROL FOR TAIL BUFFET ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION
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