Single-level composite wing optimization based on flexural lamination parameters

Structural and Multidisciplinary Optimization

Volumn 26, Issue 1-2, 2004, Pages 111-120

  Liu, B ^a   Haftka, R T ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

Buckling load; Combinatorial optimization; Composite laminate; Composite wing structures; Discrete design variables; Flexural lamination parameters; Genetic algorithms; Response surface; Stacking sequence optimization; Two level optimization

Indexed keywords

APPROXIMATION THEORY; FIBER REINFORCED MATERIALS; GENETIC ALGORITHMS; LAMINATES; PROBLEM SOLVING; STIFFNESS MATRIX; STRUCTURAL ANALYSIS; THICKNESS MEASUREMENT;

BUCKLING LOAD; COMBINATORIAL OPTIMIZATION; COMPOSITE LAMINATES; COMPOSITE WING STRUCTURES; RESPONSE SURFACE; STACKING SEQUENCE OPTIMIZATION; TWO-LEVEL OPTIMIZATION;

STRUCTURAL OPTIMIZATION;

EID: 1142276168     PISSN: 1615147X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00158-003-0315-6     Document Type: Article

References (14)

1. Fukunaga, H.; Sekine, H. 1992: Stiffness design method of symmetrical laminates using lamination parameters, AIAA J. 30(11), 2791-2793
2. Fukunaga, H.; Sekine, H. 1994: Laminate design for elastic properties of symmetric laminates with extension-shear or bending-twisting coupling, J. Compos. Mater. 28(8), 708-731
3. Lekhnitskii, S.G. 1968: Anisotropic Plates. London: Gordon and Breach Sci. Publ.; translated by Tsai, S.W. and Cheron, T.
4. Liu, B.; Haftka, R.T.; Akgün, M. 2000: Two-level composite wing structural optimization using response surfaces. J. Struct. Multidisc. Optim. 20, 87-96
5. Liu, B.; Haftka, R.T.; Akgün, M.; Todoroki, A. 2000: Permutation genetic algorithm for stacking sequence design of composite laminates. Comput. Methods Appl. Mech. Eng. 186, 357-372; special issue edited by Goldberg, D. and Kalyanmoy, D.
6. Liu, B.; Haftka, R.T.; Trompette, P. 2003: Maximization of buckling loads of composite panels using flexural lamination parameters. J. Struct. Multidisc. Optim. 25, 1-9
7. Miki, M. 1986: Optimum design of laminated composite plates subject to axial compression. In: Kawata, K.; Ume-Kawa, S.; Kobayashi, A. (eds.) Composites' 86: Recent Advances in Japan and the United States, Proc. Japan-U.S. CCM-III (held in Tokyo), pp. 673-680
8. Miki, M.; Sugiyama, Y. 1991: Optimum design of laminated composite plates using lamination parameters. In: Proc. /ASME/ASCE/AHS/ASC 32nd Structures, Structural Dynamics and Materials Conference (held in Washington, DC), AIAA Paper AIAA-91-0971, pp. 275-283
9. Miki, M.; Sugiyama, Y. 1993: Optimum design of laminated composite plates using lamination parameters. AIAA J. 31(5), 921-922
10. Tsai, S.W.; Pagano, N.J. 1968: Invariant properties of composite materials. In: Tsai, S.W.; Halpin, J.C.; Pagano, N.J. (eds.) Composite Materials Workshop, pp. 233-253. Westport: Technomic Publishing
11. Tsai, S.W.; Hahn, H.T. 1980: Introduction of Composite Materials. Lancaster: Technomic
12. Vanderplaats Research and Development, Inc. 2000: GENESIS User Manual, Version 6.0. Colorado Springs, CO80906
13. Whitney, J.M. 1985: Structural Analysis of Laminated Anisotropic Plates. Lancaster: Technomic
14. Yamazaki, K. 1996: Two-level optimization technique of composite panels by genetic algorithm. In: Proc. 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material Conference (held in Salt Lake City), Part 4, AIAA Paper 96-153, pp. 1882-1886