Helicopter Tail Rotor Thrust and Main Rotor Wake Coupling in Crosswind Flight
- 1 November 2010
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 47 (6), 2136-2148
- https://doi.org/10.2514/1.c031018
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- A Rational Approach to Comparing the Performance of Coaxial and Conventional RotorsJournal of the American Helicopter Society, 2010
- Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flightThe Aeronautical Journal, 2009
- Wake Dynamics and Rotor-Fuselage Aerodynamic InteractionsJournal of the American Helicopter Society, 2009
- Main Rotor-Tail Rotor Interaction and Its Implications for Helicopter Directional ControlJournal of the American Helicopter Society, 2008
- Efficient High-Resolution Wake Modeling Using the Vorticity Transport EquationAIAA Journal, 2005
- Rotor Wake Modeling for Flight Dynamic Simulation of HelicoptersAIAA Journal, 2000
- Lynx Main Rotor/Tail Rotor Interactions: Mechanisms and ModellingProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 1994
- Tail Rotor Performance in Presence of Main Rotor, Ground, and WindsJournal of the American Helicopter Society, 1974
- A Note on a Phenomenon Affecting Helicopter Directional Control in Rearward FlightJournal of the American Helicopter Society, 1970
- Tail Rotor Design Part I: AerodynamicsJournal of the American Helicopter Society, 1970