Approximate method for the optimum design of ring and stringer stiffened cylindrical panels and shells with local, inter-ring, and general buckling modal imperfections
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Publication:4214320
DOI10.1016/0045-7949(95)00264-2zbMath0919.73084OpenAlexW2087930702MaRDI QIDQ4214320
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Publication date: 6 September 1999
Published in: Computers & Structures (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7949(95)00264-2
Bifurcation and buckling (74G60) Optimization problems in solid mechanics (74P99) Software, source code, etc. for problems pertaining to mechanics of deformable solids (74-04)
Related Items (4)
ON THE USE OF GENERALIZED BEAM THEORY TO ASSESS THE BUCKLING AND POSTBUCKLING BEHAVIOR OF LAMINATED CFRP CYLINDRICAL STIFFENED PANELS ⋮ Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime ⋮ On a stress resultant geometrically exact shell model. III: Computational aspects of the nonlinear theory ⋮ A SYMPLECTIC HAMILTONIAN APPROACH FOR THERMAL BUCKLING OF CYLINDRICAL SHELLS
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