Minimum Weight Design of Stiffened Fiber Composite Cylinders
- 1 July 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (7) , 562-569
- https://doi.org/10.2514/3.59138
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Minimum Weight Design of Stiffened Fiber Composite CylindersJournal of Aircraft, 1971
- Structural synthesis of integrally stiffened cylinders.Journal of Spacecraft and Rockets, 1968
- Structural synthesis capability for integrally stiffened waffle platesAIAA Journal, 1963
- A Rapidly Convergent Descent Method for MinimizationThe Computer Journal, 1963
- STABILITY OF HETEROGENEOUS AEOLOTROPIC CYLINDRICAL SHELLS UNDER COMBINED LOADINGAIAA Journal, 1963