An approach to the development of durable and damage tolerant composite commercial aircraft structure
- 24 March 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Early Detection of Fatigue Damage in Composite MaterialsJournal of Aircraft, 1976
- Measurement of fatigue damage in composite materialsExperimental Mechanics, 1975
- Microcrack Growth in Graphite Fiber-Epoxy Resin Systems During Compressive FatiguePublished by ASTM International ,1975