Helicopter Noise: State-of-the-Art
- 1 November 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (11), 707-715
- https://doi.org/10.2514/3.58436
Abstract
No abstract availableKeywords
This publication has 47 references indexed in Scilit:
- Effect of the incident surface pressure field on noise due to turbulent flow past a trailing edgeJournal of Sound and Vibration, 1978
- High-Frequency Broadband Rotor NoiseAIAA Journal, 1977
- Noise Produced by Turbulent Flow into a Propeller or Helicopter RotorAIAA Journal, 1977
- Numerical Calculation of Unsteady Transonic Potential Flow over Helicopter Rotor BladesAIAA Journal, 1976
- Experimental Evaluation of Theories for Trailing Edge and Incidence Fluctuation NoiseAIAA Journal, 1975
- Prediction of airfoil tone frequenciesJournal of Aircraft, 1975
- Isolated Airfoil-Tip Vortex Interaction NoiseJournal of Aircraft, 1975
- Vortex Noise of Isolated AirfoilsJournal of Aircraft, 1973
- Aerodynamic Sound Due to a Source Near a Half-PlaneIMA Journal of Applied Mathematics, 1972
- Vortex flow over helicopter rotor tipsJournal of Aircraft, 1971