Rotating-Blade Vortex Noise

SM_VSTOL_1972-4110

10/26/1972

Authors
Abstract
Content

An experimental investigation has been made in the Langley full-scale tunnel and outdoors to investigate some of the characteristics of vortex noise generated on a rotating-blade system. Acoustic measurements were made at several microphone positions for two different blade sections with several tip shapes and spoiler configurations. The blades were operated only at zero lift at each radial station, both for operating in their own wake and for operating with the wake blown downstream. The rotors with cylindrical blades generally created more noise throughout the noise spectrum than the rotor with NACA 0012 blades. Blowing the shed wake from the rotor with cylindrical blades did not have an appreciable effect on the frequency-amplitude spectrum. The tip shape changes had very little effect on the frequency-amplitude spectrum of the noise. Spoilers applied to the rotor with NACA 0012 blades increased the amplitude of the spectrum and decreased. the number of harmonics of blade passage frequency. Blowing the shed wake away from the rotor with NACA 0012 blades had an appreciable effect on the spectrum in that the broad band noise and the presence of the number of harmonics of blade passage frequency were greatly decreased.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_VSTOL_1972-4110
Citation
Scheiman, J., Letko, W., Shivers, J., and Hilton, D., "Rotating-Blade Vortex Noise," Symposium on Status of Testing and Modeling Techniques for V/STOL Aircraft, Philadelphia 1972, Philadelphia, Pennsylvania, October 26, 1972, https://doi.org/10.4050/SM_VSTOL_1972-4110.
Additional Details
Publisher
Published
10/26/1972
Product Code
SM_VSTOL_1972-4110
Content Type
Technical Paper
Language
English