Minimum Weight Analysis Based on Structural Reliability
- 1 September 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (9) , 641-652
- https://doi.org/10.2514/8.8702
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal PressureJournal of the Aeronautical Sciences, 1957