Performance Measurement and Wake Characteristics of a Model Rotor in Axial Flight
- 1 April 1999
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 44 (2), 101-108
- https://doi.org/10.4050/jahs.44.101
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Challenges in Understanding the Vortex Dynamics of Helicopter Rotor WakesAIAA Journal, 1998
- Aerodynamic aspects of blade-vortex interaction (BVI)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Rotor tip-vortex/airframe collision featuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Wake-vortex separation distances when flight-path corridors are constrainedJournal of Aircraft, 1996
- Performance results from a test of an S-76 rotor in the NASA Ames 80- by 120-foot wind tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Flowfield of a swept blade tip at high pitch anglesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Special Vortices at a Helicopter Rotor BladeJournal of the American Helicopter Society, 1990
- Measurement of the interaction between a rotor tip vortex and a cylinderAIAA Journal, 1990
- Visualization and measurement of the tip vortex core of a rotor blade in hoverJournal of Aircraft, 1988
- Prediction of Aeroelastic Response of a Model X-Wing RotorJournal of the American Helicopter Society, 1987