Helicopter Main-Rotor/Tail-Rotor Interaction
- 1 October 2000
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 45 (4), 293-302
- https://doi.org/10.4050/jahs.45.293
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Aerodynamics and aeroacoustics of helicopter main-rotor/tail-rotor interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Unsteady Panel Method Calculation of Pressure Distribution on BO 105 Model Rotor BladesJournal of the American Helicopter Society, 1998
- An analytical model for the prediction of MR/TR interaction noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Potential flow about three-dimensional lifting configurations, with application to wings and rotorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Nonlinear two-dimensional unsteady potential flow with lift.Journal of Aircraft, 1968
- Calculation of potential flow about arbitrary bodiesProgress in Aerospace Sciences, 1967