The acoustic results of a United Techologies scale model helicopter rotor tested at DNW
- 17 August 1990
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A prediction of high-speed rotor noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Experimental and analytical aerodynamics of an advanced rotor in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- The spectral characteristics of rotor blade-vortex interaction noise- Experimental and mathematical resultsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Helicopter impulsive noise: Theoretical and experimental statusJournal of Sound and Vibration, 1986