Interval Finite Element Analysis of Wing Flutter
نویسندگان
چکیده
منابع مشابه
Flutter Analysis of a Low Aspect Ratio Swept- Back Trapezoidal Wing at Low Subsonic Flow
A linear, aeroelastic analysis of a low aspect ratio swept back trapezoidal wing modeled as a cantilever plate is presented. An analytical and numerical formulation for both the aerodynamic forcing and structural response of the wing was developed. The analytical model uses a three dimensional time domain vortex lattice aerodynamic method. A Rayleigh-Ritz approach has been used to transfer equa...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2008
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(08)60017-5