Design of frames against buckling using a Rayleigh quotient approximation
- 1 June 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (6) , 1143-1149
- https://doi.org/10.2514/3.11739
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- High-quality approximation of eigenvalues in structural optimizationAIAA Journal, 1990
- Exploratory design studies using an integrated multidisciplinary synthesis capability for actively controlled composite wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Improved Approximations for Control Augmented Structural SynthesisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Bimodal optimization of frames for maximum stabilityComputers & Structures, 1989
- An efficient approximation technique for frequency constraints in frame optimizationInternational Journal for Numerical Methods in Engineering, 1988
- Optimization of Shallow Trusses Against Limit Point InstabilityAIAA Journal, 1984
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979
- On single and bimodal optimum buckling loads of clamped columnsInternational Journal of Solids and Structures, 1977
- Optimum structural design with stability constraintsInternational Journal for Numerical Methods in Engineering, 1976