Vortex induced helicopter blade loads and noise
- 1 April 1973
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 27 (3), 387-398
- https://doi.org/10.1016/s0022-460x(73)80353-0
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971
- Approximate transfer functions for large aspect ratio wings in turbulent flowJournal of Aircraft, 1971
- A lifting-surface solution for vortex-induced airloadsAIAA Journal, 1971
- Similarity rules for thin aerofoils in non-stationary subsonic flowsJournal of Fluid Mechanics, 1970
- Direct Correlation of Fluctuating Lift with Radiated Sound for an Airfoil in Turbulent FlowThe Journal of the Acoustical Society of America, 1969
- A theoretical study of helicopter rotor noiseJournal of Sound and Vibration, 1969
- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941