Convergence-Proof of Discrete-Panel Wing Loading Theories
- 1 October 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (10) , 837-839
- https://doi.org/10.2514/3.59178
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Skin-Friction Formula for Tapered and Delta WingsJournal of Aircraft, 1969
- Some effects of planform modification on the skin friction dragAIAA Journal, 1964