Tail Buffet Alleviation of High Performance Twin Tail Aircraft Using Piezo-Stack Actuators
Conference, Structures, structural materials and dynamics ; 1999 ; St Louis; MO
1999-01-01
11 pages
Nos 99-1202 to 99-1613 with gaps
Aufsatz (Konferenz)
Englisch
structures , AIAA , ASME , ASCE
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VORTEX CONTROL FOR TAIL BUFFET ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION
SAE Technical Papers | 1989
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