Simultaneous cost and weight minimization of postbuckled composite panels under combined compression and shear
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[1] Asme,et al. A collection of technical papers : 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 18-20, 1994, Hilton Head, SC , 1994 .
[2] Garret N. Vanderplaats,et al. CONMIN: A FORTRAN program for constrained function minimization: User's manual , 1973 .
[3] L. Ilcewicz,et al. The use of COSTADE in developing composite commercial aircraft fuselage structures , 1994 .
[4] Christos Kassapoglou,et al. Minimum cost and weight design of fuselage frames. Part B : cost considerations, optimization, and results , 1999 .
[5] Christos Kassapoglou. Minimum cost and weight design of fuselage frames: Part A: design constraints and manufacturing process characteristics , 1999 .
[6] Christos Kassapoglou,et al. Simultaneous cost and weight minimization of composite-stiffened panels under compression and shear , 1997 .
[7] Erdogan Madenci,et al. DESIGN METHODOLOGY AND LIFE ANALYSIS OF POSTBUCKLED METAL AND COMPOSITE PANELS. , 1985 .
[8] P. Hajela,et al. MULTICRITERION DESIGN OF FUZZY STRUCTURAL SYSTEMS USING IMMUNE NETWORK SIMULATION , 1999 .
[9] G. Vanderplaats,et al. Structural optimization by methods of feasible directions. , 1973 .