Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints
نویسندگان
چکیده
منابع مشابه
The AVINOR Aeroelastic Simulation Code and its Application to Reduced Vibration Composite Rotor Blade Design
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2004
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(11)60230-6