Structural Optimization of a Thick-Walled Composite Multi-Cell Wing Box Using an Approximation Method |
Kim, San-Hui
(Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Kim, Pyung-Hwa (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University) Kim, Myung-Jun (Department of Aviation Maintenance Engineering, Silla University) Park, Jung-sun (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) |
1 | C. Kim, S. R. White, "Thick-Walled Composite Beam Theory including 3-D Elastic effects and torsional warping," lnl. J. Solids Structures Vol. 34, Nos 31-32, pp. 4237-4259, 1997. |
2 | V. V. Vasiliev, E. V. Morozov, Advanced Mechanics of composite materials and structural elements, 3rd Edition., ELSVIER 2013. |
3 | E. C. Smith, "Formulation and evaluation of an analytical model for composite box-beams," J. Am. Helicopt. Soc. 36, pp. 23-35, 1991. DOI |
4 | R. Chandra, I. Chopr, "Thin-walled composite beams under bending, torsional, and extensional loads," Journal of Aircraft, Vol. 27, No.7, July, pp.619-626, 1990. DOI |
5 | A. Vincenti, A Two- step optimisation approach for the design of composite stiffende panels partI: global structural optimisation, version 1 - 10 Nov 2011. |
6 | J. M. Whitney, Structural Analysis of Laminated Anisotropic Plates, TECHNOMIC. 1987. |
7 | C. T. Herakovich, Mechanics of Fibrous Composites, John Wiley & Sons, Inc. 1998. |