Structural optimization and design based on a reliability design criterion
- 1 January 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 1 (1) , 56-61
- https://doi.org/10.2514/3.27592
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Minimum Weight Analysis Based on Structural ReliabilityJournal of the Aerospace Sciences, 1960