Equivalent Plate Modeling of the Wing-Box Structure with Control Surface

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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.
Publisher
한국항공우주학회
Issue Date
2006-11
Language
ENG
Citation

KSAS INTERNATIONAL JOURNAL, v.7, no.2, pp.104 - 109

ISSN
2093-274X
URI
http://hdl.handle.net/10203/5728
Appears in Collection
AE-Journal Papers(저널논문)

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