Equivalent Plate Modeling of the Wing-Box Structure with Control Surface
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
- English
- Citation
KSAS INTERNATIONAL JOURNAL, v.7, no.2, pp.104 - 109
- ISSN
- 2093-274X
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.