Aerodynamic Results of a Pressure‐Instrumented Model Rotor Test at the DNW
- 1 October 1991
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 36 (4) , 66-76
- https://doi.org/10.4050/jahs.36.66
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The acoustic results of a United Techologies scale model helicopter rotor tested at DNWPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- A prediction of high-speed rotor noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Airfoil dynamic stall at constant pitch rate and high Reynolds numberJournal of Aircraft, 1988
- An experimental study of rotor-vortex interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- An Analytical Method for Predicting Rotor Wake GeometryJournal of the American Helicopter Society, 1969