Wing box optimization under combined shear and bending.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 3 (2) , 130-141
- https://doi.org/10.2514/3.43717
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Principles of Structural Design for Minimum WeightJournal of the Aeronautical Sciences, 1949