Combined loads minimum weight analysis of stiffened plates and shells.
- 1 February 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (2) , 235-240
- https://doi.org/10.2514/3.28425
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLSAIAA Journal, 1963
- THE MINIMUM WEIGHT DESIGN OF STRUCTURES OPERATING IN AN AEROSPACE ENVIRONMENTPublished by Defense Technical Information Center (DTIC) ,1962