Multiple-Surrogate Approach to Helicopter Rotor Blade Vibration Reduction

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Multiple-Surrogate Approach to Helicopter Rotor Blade Vibration Reduction

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ژورنال

عنوان ژورنال: AIAA Journal

سال: 2009

ISSN: 0001-1452,1533-385X

DOI: 10.2514/1.40291