Maximization of buckling loads of composite panels using flexural lamination parameters

Structural and Multidisciplinary Optimization

Volumn 26, Issue 1-2, 2004, Pages 28-36

  Liu, B ^a   Haftka, R T ^a   Trompette, P ^b  

^a UNIVERSITY OF FLORIDA   (United States)

^b INSERM   (France)

Author keywords

Buckling load; Combinatorial optimization; Composite laminate; Discrete design variables; Flexural lamination parameters; Genetic algorithms; Stacking sequence optimization

Indexed keywords

ASPECT RATIO; COMPUTATIONAL METHODS; GENETIC ALGORITHMS; LAMINATING; PROBLEM SOLVING; STIFFNESS; STRUCTURAL OPTIMIZATION;

BUCKLING LOAD; COMBINATORIAL OPTIMIZATION; COMPOSITE LAMINATES; DISCRETE DESIGN VARIABLES; FLEXURAL LAMINATION PARAMETERS; STACKING SEQUENCE OPTIMIZATION;

FIBER REINFORCED MATERIALS;

EID: 1142264040     PISSN: 1615147X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00158-003-0314-7     Document Type: Article

References (17)

1. Diaconu, C.G.; Sato, M.; Sekine, H. 2002: Feasible region in general design space of lamination parameters of laminated composites. AIAA J. 50(3), 559-565
2. Fukunaga, H.; Sekine, H. 1992: Stiffness design method of symmetrical laminates using lamination parameters. AIAA J. 30(11), 2791-2793
3. 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
4. Grenestedt, J.L.; Gudmundson, P. 1993: Layup optimization of composite material structures. In: Pedersen, P. (ed.) Optimal Design with Advanced Materials, pp. 311-336
5. Haftka, R.T.; Walsh, J.L. 1992: Stacking sequence optimization for buckling of laminated plates by integer programming. AIAA J. 30(3), 814-819
6. Lekhnitskii, S.G. 1968: Anisotropic Plates. London: Gordon and Breach Sci. Publ.; translated by Tsai, S.W. and Cheron, T.
7. Liu, B.; Haftka, R.T.; Akgün, M. 2000: Two-level composite wing structural optimization using response surfaces. J. Struct. Multidisc. Optim. 20, 87-96
8. 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
9. 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
10. Miki, M.; Sugiyama, Y. 1991: Optimum design of laminated composite plates using lamination parameters. In: Proc. AIAA/ASME/ASCE/AHS/ASC 32nd Structures, Structural Dynamics and Materials Conference (held in Washington, DC), AIAA Paper AIAA-91-0971, pp. 275-283
11. Miki, M.; Sugiyama, Y. 1993: Optimum design of laminated composite plates using lamination parameters. AIAA J. 31(5), 921-922
12. 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
13. Tsai, S.W.; Hahn, H.T. 1980: Introduction of Composite Materials. Lancaster: Technomic
14. Todoroki, A.; Haftka, R.T. 1998: Lamination parameters for efficient genetic optimization of the stacking sequences of composite panels. In: Proc. 7th AIAA/USAF/NASA/ISSMO Multidisciplinary Analysis and Optimization Symposium (held in St. Louis), AIAA-98-4816, pp. 870-879
15. Vanderplaats Research and Development, Inc. 1995: DOT User Manual, Version 4.20
16. Whitney, J.M. 1985: Structural Analysis of Laminated Anisotropic Plates. Lancaster: Technomic
17. 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