Design for temperature and thermal buckling constraints employing a noneigenvalue formulation
- 1 July 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 20 (4) , 363-367
- https://doi.org/10.2514/3.25607
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Preflight reentry heat transfer analysis of Space ShuttlePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979
- Optimum Design of Structures at Elevated TemperaturesAIAA Journal, 1979
- A general variational principle for thermal insulation system designInternational Journal of Heat and Mass Transfer, 1979
- Structural optimization: A review and some recommendationsInternational Journal for Numerical Methods in Engineering, 1978
- Optimization of flexible wing structures subject to strength and induced drag constraintsAIAA Journal, 1977
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976
- A Polyalgorithm for the Numerical Solution of Ordinary Differential EquationsACM Transactions on Mathematical Software, 1975
- A cylindrical shell discrete element.AIAA Journal, 1967