Recent developments in rotary-wing aerodynamic theory
Author:
- 1 August 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (8) , 1219-1244
Abstract
No abstract availableKeywords
This publication has 49 references indexed in Scilit:
- SUBSONIC PANEL METHODS - A COMPARISON OF SEVERAL PRODUCTION CODES1985
- Compressible lifting surface theory for propeller performance calculationJournal of Aircraft, 1985
- Compressible Helicoidal Surface Theory for Propeller Aerodynamics and NoiseAIAA Journal, 1983
- Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel MethodsJournal of Aircraft, 1982
- The Prediction of Clmax Using a Separated Flow ModelJournal of the American Helicopter Society, 1978
- A Simplified Approach to Generalized Helicopter Configuration Modeling and the Prediction of Fuselage Surface PressuresJournal of the American Helicopter Society, 1976
- Potential flow about three-dimensional lifting configurations, with application to wings and rotors1975
- Nonlinear Helicopter Rotor Lifting Surface Theory. Part I1973
- A numerical method for the calculation of nonlinear, unsteady lifting potential flow problemsAIAA Journal, 1969
- Kernel Function for Nonplanar Oscillating Surfaces in a Subsonic FlowAIAA Journal, 1967