Loss in Aileron Effectiveness Because of Wing Twist and Considerations Regarding the Internal-Pressure Balanced Aileron
- 1 January 1944
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 11 (1) , 41-47
- https://doi.org/10.2514/8.11091
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Graphic Determination of Distance in Accelerated Airplane MotionJournal of the Aeronautical Sciences, 1943
- The Prediction of PerformanceAircraft Engineering and Aerospace Technology, 1940
- Critical Speeds of MonoplanesJournal of the Royal Aeronautical Society, 1937