The Second-Order Lifting Pressure and Damping in Roll of Sweptback Rolling Airfoils at Supersonic Speeds
- 1 October 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (10) , 699-704
- https://doi.org/10.2514/8.2798
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On the Pure Rolling Motion of Winged And/Or Finned Missiles in Varying Supersonic FlightJournal of the Aeronautical Sciences, 1953
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951
- Supersonic Wave Drag of Thin AirfoilsJournal of the Aeronautical Sciences, 1946