Lifting-Line Analysis for Twisted Wings and Washout-Optimized Wings
- 1 January 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 41 (1) , 128-136
- https://doi.org/10.2514/1.262
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Three-Dimensional Small-Disturbance SolutionsPublished by Cambridge University Press (CUP) ,2001
- Lifting-Line Theory for Arbitrarily Shaped WingsJournal of Aircraft, 1999
- Solution of the lifting line equation for twisted elliptic wingsJournal of Aircraft, 1971