Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime
DOI10.1016/0045-7825(93)90041-UzbMath0825.73457OpenAlexW2012196825MaRDI QIDQ1209963
Publication date: 16 May 1993
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7825(93)90041-u
Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Optimization problems in solid mechanics (74P99) Software, source code, etc. for problems pertaining to mechanics of deformable solids (74-04)
Uses Software
Cites Work
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- Some computational aspects of the stability analysis of nonlinear structures
- Nonlinear equilibrium of imperfect, locally deformed stringer-stiffened panels under combined in-plane loads
- Computerized analysis of shells-governing equations
- Postbuckling behavior of anisotropic laminated plates under pure shear and shear combined with compressive loading
- A Curved C0 Shell Element Based on Assumed Natural-Coordinate Strains
- A general-purpose optimization program for engineering design
- PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels
- Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads
- A numerical and experimental investigation of the buckling behavior of composite panels
- Panda—Interactive program for minimum weight design of stiffened cylindrical panels and shells
- 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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