ACTIVE VORTICAL FLOW CONTROL FOR ALLEVIATION OF TWIN-TAIL BUFFET OF GENERIC FIGHTER AIRCRAFT
38th, Aerospace sciences meeting ; 2000 ; Reno, NV
2000-01-01
ALL
Paper nos AIAA-2000-0001 to AIAA-2000-1076 with gaps
Aufsatz (Konferenz)
Englisch
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