On sound generated when a vortex is chopped by a circular airfoil-Reference-Cited by-同舟云学术

On sound generated when a vortex is chopped by a circular airfoil

Published:1989-02 Issue:3 Volume:128 Page:487-503
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Howe M.S.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference16 articles.

1. Helicopter impulsive noise: theoretical and experimental status;Schmitz,1986

2. Main rotor/tail rotor interactions;Leverton;Vertica,1977

3. Rotor-vortex interaction noise;Schlinker;American Institute of Aeronautics and Astronautics, Paper 83-0720,1983

4. An experimental investigation of blade-vortex interaction at normal incidence;Ahmadi;American Institute of Aeronautics and Astronautics, Journal of Aircraft,1986

5. C. M. CaryNASA Contractor Report No. CR-177457. An experimentalinvestigation of the chopping of helicopter main rotor tip vortices by the tail rotor. Part II: High speed photographic study.

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