AIAA-2006-1821 Surrogate Based Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
01.01.2006
21 pages
Paper numbers 2006-1600 to 2006-2284 with gaps held
Aufsatz (Konferenz)
Englisch
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Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
British Library Conference Proceedings | 2006
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