Analysis and Testing of a Mach Scaled Rotor Model with Piezoelectric Bender Actuated Trailing-Edge Flaps for Helicopeter Vibration Control
Conference, Structures, structural materials and dynamics ; 1999 ; St Louis; MO
01.01.1999
23 pages
Nos 99-1202 to 99-1613 with gaps
Aufsatz (Konferenz)
Englisch
structures , AIAA , ASME , ASCE
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