Approach for analysis and design of composite rotor blades
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (4), 693-697
- https://doi.org/10.2514/3.46221
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A study of three‐node triangular plate bending elementsInternational Journal for Numerical Methods in Engineering, 1980