[KSCI] Korea Science Citation Index Service

http://dx.doi.org/10.5139/IJASS.2006.7.2.104

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

Kim, Eun-Ho
Roh, Jin-Ho
Yoo, Seung-Jae
Lee, In

Publication Information

International Journal of Aeronautical and Space Sciences / v.7, no.2, 2006 , pp. 104-109 More about this Journal

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.

Keywords

Equivalent plate; Wing structure; Control surface;

Citations & Related Records

Reference

1	Kim, D. K., 'Dynamic Characteristics and Model Establishment of Deployable Missile Control Fin with Nonlinear Hinge,' M.S. Thesis, Dept. of Mechanical Engineering Div. of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 2003
2	Han, J. H.,'Flutter Analysis of Aircraft Wing Using Equivalent Structural Model,' M.S. Thesis, Dept. of Mechanical Engineering Div. of Aerospace Engineering, Korea Advanced Institute of Science and Technology., 1999
3	Livne, E., Sels, R A., Bhatia, K. G.,'Lessons from Application of Equivalent Plate Structural Modeling to an HSCT Wing,' Journal of Aircraft, Vol 31,No. 4, 1994, pp. 953-960 DOI ScienceOn
4	Dawe, D. J., 'Bucling and Vibration of Plate Structures Including Shear Deformation and Related Effects,' Aspects of the Analysis of Plate Structures, edited by D.l. Dawe, R W. Horsington, A. G. Kamtekar, and G. H. Little, Oxford Univ. Press, New York, 1985, pp. 75-99
5	Reddy, J. N., and Miravete, A., Practical Analysis of Composite Laminates, CRC Press, Boca Raton, FL, 1955, pp. 52-62
6	Kapania, R. K., Raciti, S., 'Recent Advances in Analysis of Laminated Beams and Plates, Part I: Shear Effects and Bucking,'AlAA Journal, Vol. 27, No.7, 1989, pp. 923-934
7	Knight, N. F., Qi, Y., 'On a Consistent First-Order Shear Deformation Theory for Laminated Plates,' Composites Part B: Engineering, Vol. 28B, 1997, pp. 397-405
8	Kapania R.K., Liu Y., 'Static and Vibration Analysis of General Wing Structures Using Equivalent-Plate Models,' AlAA Journal, Vol. 38, No.7, 2000, pp. 1269-1277