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. Flutter analysis will be conducted for a truss-braced wing aircraft concept with tension stiffening and inertial force coupling.
Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft
AIAA SciTech 2016 ; 2016 ; San Diego, CA, United States
2016-01-04
Aufsatz (Konferenz)
Keine Angabe
Englisch
Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft (AIAA 2016-1094)
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