Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft
نویسندگان
چکیده
This paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircraft. The geometric are nonlinearity due to rotational and tension stiffening. The effect of large bending deflection will also be investigated. Aeroelastic analysis will be conducted for a truss-braced wing aircraft concept with nonlinear effect of large bending deflection and inertial force coupling.
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