An efficient and robust method for predicting helicopter rotor high-speed impulsive noise
- 15 January 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Acoustic Predictions Using Measured Pressures from a Model Rotor in the DNWJournal of the American Helicopter Society, 1993
- The Uses and Abuses of the Acoustic Analogy in Helicopter Rotor Noise PredictionJournal of the American Helicopter Society, 1988
- The importance of quadrupole sources in prediction of transonic tip speed propeller noiseJournal of Sound and Vibration, 1979
- Sound generation by turbulence and surfaces in arbitrary motionPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1969
- On sound generated aerodynamically II. Turbulence as a source of soundProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1954
- On sound generated aerodynamically I. General theoryProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1952