Helicopter Vibration Reduction in Forward Flight using Blade Integral Twist Control
43rd, Structures, structural dynamics, and materials conference; 10th AIAA/ASME/ASCE/AHS adaptive structures forum, 4th AIAA non-deterministic approaches forum, 3rd AIAA gossamer spacecraft forum ; 2002 ; Denver, CO
2002-01-01
10 pages
Conference paper
English
structural dynamics , materials , AHS , gossamer spacecraft , AMSE , ASCE , structures , adaptive structures , AIAA , ASC
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Helicopter vibration reduction in forward flight using blade integral twist control
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