Boundary-element shape optimization system for aircraft structural components
- 1 July 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (7), 1203-1204
- https://doi.org/10.2514/3.25194
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Design‐Sensitivity analysis of Solids Using BEMJournal of Engineering Mechanics, 1988