Preliminary design of composite wing-box structures for global damage tolerance
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Recent Developments in the Design, Testing and Impact-Damage Tolerance of Stiffened Composite PanelsPublished by Springer Nature ,1980
- 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
- Vulnerability Analysis of Optimized StructuresAIAA Journal, 1978
- An approach to the development of durable and damage tolerant composite commercial aircraft structurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Damage tolerance assessment of F-4 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Rapid analysis of damaged structureAIAA Journal, 1976
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976