Angle of Attack Increase of an Airfoil in Decelerating Flow
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (7) , 506-507
- https://doi.org/10.2514/3.59024
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Some Simplified Methods in Airfoil TheoryJournal of the Aeronautical Sciences, 1942