×

A multicriteria objective function optimization scheme for laminated composites for use in multilevel structural optimization schemes. (English) Zbl 0587.73137

A multilevel optimization scheme for large laminated composite structures is proposed, and a suitable element/lower-level optimization scheme using a multicriteria objective function is developed. The objective function combines a weight function and a strain energy change function into a utility function which is minimized and in which the relative importance of each part is reflected by weighting coefficients. Minimizing the change in strain energy ensures load path continuity in the overall structure when switching between upper and lower levels of optimization, and so decouples the problems at the two levels. Continuous lamina thickness and ply-angle variation is used to minimize the objective function while satisfying strain, buckling, and gauge constraints. Numerical applications are given to illustrate the effect of the weighting coefficients in the objective function on the final result, and to demonstrate the algorithm’s effectiveness as a pure weight minimization routine.

MSC:

74P99 Optimization problems in solid mechanics
74E30 Composite and mixture properties
Full Text: DOI

References:

[1] Schmit, L. A.; Farshi, B., Optimum laminate design for strength and stiffness, Internat. J. Numer. Meths. Engrg., 7, 519-536 (1973)
[2] Massard, T. N., Computer sizing of composite laminates for strength, J. Reinf. Plastics Composites, 3, 300-345 (1984)
[3] Flanagan, G. N., Development and application of optimization techniques for composite laminates, (M.Sc. Thesis, AFIT/GAE/AA/83S-4 (1983), Airforce Institute: Airforce Institute OH)
[4] Park, W. J., An optimal design of simple symmetric laminates under first ply failure criterion, J. Composite Materials, 16, 341-345 (1982)
[5] Schmit, L. A.; Farshi, B., Optimum design of laminated composite plates, Internat. J. Numer. Meths. Engrg., 11, 623-640 (1977) · Zbl 0356.73054
[6] Tauchert, T. R.; Adibhatla, S., Design of laminated plates for maximum stiffness, J. Composite Materials, 18, 58-69 (1984)
[7] Tauchert, T. R.; Adibhatla, S., Design of laminated plates for maximum bending strength, Engrg. Optim., 8, 253-263 (1985)
[8] Stroud, W. J.; Agranoff, N., Minimum-mass design of filamentary composite panels under combined loads: Design procedure based on simplified buckling equations, (NASA TN D-8257 (1976), NASA Langley Research Center: NASA Langley Research Center Hampton, VA)
[9] Stroud, W. J.; Agranoff, N.; Anderson, M. S., Minimum-mass design of filamentary composite panels under combined loads: Design procedure based on a rigorous buckling analysis, (NASA TN D-8257 (1976), NASA Langley. Research Center: NASA Langley. Research Center Hampton, VA)
[10] Adali, S., Multiobjective design of an antisymmetric angle-ply laminate by non-linear programming, ASME J. Mechanisms, Transmissions, Automation Design, 105, 214-219 (1983)
[11] Khot, N. S., Computer program (OPTCOMP) for optimization of composite structures for minimum weight design, (AFFDL TR-76-149 (1977), Wright-Patterson Air Force Base: Wright-Patterson Air Force Base Dayton, OH)
[12] McKeown, J. J., Optimal composite structures by deflection-variable programming, Comput. Meths. Appl. Mech. Engrg., 12, 155-179 (1977) · Zbl 0368.90132
[13] Starnes, J. H.; Haftka, R. T., Preliminary design of composite wings for buckling, strength and displacement constraints, (Proceedings 19th AIAA, ASME Structures, Structural Dynamics and Materials Conference. Proceedings 19th AIAA, ASME Structures, Structural Dynamics and Materials Conference, Bethesda, MD (1978))
[14] Schmit, L. A.; Mehrinfar, M., Multilevel optimum design of structures with fibre-composite stiffened-panel components, AIAA J., 20, 138-147 (1982) · Zbl 0474.73104
[15] Sobieszczanski-Sobieski, J., An integrated computer procedure for sizing composite airframe structures, (NASA TP 1300 (1979), NASA Langley Research Center: NASA Langley Research Center Hampton, VA) · Zbl 0852.73041
[16] Schmit, L. A.; Ramanathan, R. K., Multilevel approach to minimum weight design including buckling constraints, AIAA J., 16, 97-104 (1978)
[17] Osyczka, A., Multicriterion Optimization in Engineering: With Fortran Programs (1984), Ellis Horwood: Ellis Horwood Chichester, U.K
[18] Hwang, C. L.; Paidy, S. R.; Yoon, K.; Masud, A. M., Mathematical programming with multiple objectives: A tutorial, Comput. Oper. Res., 7, 5-31 (1980)
[19] Cohon, J. L., Multiobjective Programming and Planning (1978), Academic Press: Academic Press New York · Zbl 0462.90054
[20] (Morris, A. J., Foundations of Structural Optimization: A Unified Approach (1982), Wiley: Wiley Chichester, U.K)
[21] Kirsch, U., Optimum Structural Design (1981), McGraw-Hill: McGraw-Hill New York · Zbl 0478.73083
[22] Haftka, R. T.; Kamat, M. P., Elements of Structural Optimization (1985), Martinus Nijhoff: Martinus Nijhoff The Hague · Zbl 0692.73064
[23] Jones, R. M., Mechanics of Composite Materials (1975), McGraw-Hill Kogakusha: McGraw-Hill Kogakusha Tokyo
[24] Lekhnitskii, S. G., (Anisotropic Plates (1968), Gordon and Breach: Gordon and Breach New York), (S.W. Tsai and T. Cheron, translators)
[25] Timoshenko, S., Theory of Elastic Stability (1936), McGraw-Hill: McGraw-Hill New York
[26] Allen, H. G.; Bulson, P. S., Background to Buckling (1980), McGraw-Hill: McGraw-Hill New York
This reference list is based on information provided by the publisher or from digital mathematics libraries. Its items are heuristically matched to zbMATH identifiers and may contain data conversion errors. In some cases that data have been complemented/enhanced by data from zbMATH Open. This attempts to reflect the references listed in the original paper as accurately as possible without claiming completeness or a perfect matching.