Structural Optimization of Composite Helicopter Rotor Blades with Swept Tips for Vibration Reduction in Forward Flight
5th AIAA/USAF/NASA/ISSMO symposium, Multidisciplinary analysis and optimization ; 1994 ; Panama City Beach; FL
01.01.1994
22 pages
In 2 pts
Aufsatz (Konferenz)
Englisch
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Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
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