| Equivalent Plate Modeling of the Wing-Box Structure with Control Surface
Eun-Ho Kim, Jin-Ho Roh, Seung-Jae Yoo and In Lee
International Journal of Aeronautical and Space Sicences, vol. 7, no. 2, pp.104-109, 2006
Abstract : In this study, the equivalent plate model is developed using a finite element method(FEM) based on the first order shear deformation theory(FSDT). The substructure synthesis method is used to consider the control surface. For the verification of the equivalent model, the results of free vibration analysis are compared with the ones of 3D wing structure modeled by using the MSC/NASTRAN.
Keyword : Equivalent plate, Wing structure, Control surface |
