Coupled rotor-fuselage vibration reduction using open-loop blade pitch control
نویسندگان
چکیده
منابع مشابه
Multiple-Surrogate Approach to Helicopter Rotor Blade Vibration Reduction
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ژورنال
عنوان ژورنال: Mathematical and Computer Modelling
سال: 1993
ISSN: 0895-7177
DOI: 10.1016/0895-7177(93)90109-c