The use of COSTADE in developing composite commercial aircraft fuselage structures
- 18 April 1994
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Damage tolerance design of composite structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Methodologies for optimal design of composite fuselage crown panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Including manufacturing tolerances in composite designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994