Technical Notes: Importance of an Accurate Prediction of Shock Curvature for High‐Speed Rotor Noise
- 1 January 1992
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 37 (1) , 82-85
- https://doi.org/10.4050/jahs.37.82
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Integrating the acoustic analogy for supersonic rotating surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Calculation of transonic rotor noise using a frequency domain formulationAIAA Journal, 1988
- The Uses and Abuses of the Acoustic Analogy in Helicopter Rotor Noise PredictionJournal of the American Helicopter Society, 1988
- Geometrical acoustics and transonic helicopter soundPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- The importance of quadrupole sources in prediction of transonic tip speed propeller noiseJournal of Sound and Vibration, 1979