Optimum structural design with plate bending elements - A survey
- 1 April 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (4), 517-522
- https://doi.org/10.2514/3.7789
Abstract
No abstract availableKeywords
This publication has 68 references indexed in Scilit:
- Optimum Design of Laminated Plates under Axial CompressionAIAA Journal, 1979
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979
- General Panel Sizing Computer Code and Its Application to Composite Structural PanelsAIAA Journal, 1979
- Increase of the first natural frequency and buckling load of plates by optimal fields of initial stressesActa Mechanica, 1977
- Optimal vs the Stiffened Circular PlateAIAA Journal, 1973
- Optimization of a Supersonic Panel Subject to a Flutter Constraint-A Finite-Element SolutionAIAA Journal, 1973
- Aeroelastic Optimization of a Panel in High Mach Number Supersonic FlowJournal of Aircraft, 1972
- Minimum-mass design of a plate-like structure for specified fundamental frequencyAIAA Journal, 1971
- Structural synthesis capability for integrally stiffened waffle platesAIAA Journal, 1963
- Symmetrical Bending of Circular Plates of Constant Radial Bending StressJournal of Applied Mechanics, 1962