Acoustic Predictions Using Measured Pressures from a Model Rotor in the DNW
- 1 July 1993
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 38 (3) , 35-44
- https://doi.org/10.4050/jahs.38.35
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- The acoustic results of a United Techologies scale model helicopter rotor tested at DNWPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Prediction of blade-vortex interaction noise using measured blade pressuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Helicopter Model Rotor‐Blade Vortex Interaction Impulsive Noise: Scalability and Parametric VariationsJournal of the American Helicopter Society, 1987
- Sound generation by turbulence and surfaces in arbitrary motionPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1969