Aeroacoustic Study of the Interaction of a Rotating Blade with a Batchelor Vortex-Reference-Cited by-同舟云学术

Aeroacoustic Study of the Interaction of a Rotating Blade with a Batchelor Vortex

Published:2018-02 Issue:2 Volume:56 Page:629-647
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zehner P.¹,Falissard F.²,Gloerfelt X.³

Affiliation:

1. ONERA–The French Aerospace Lab, 92322 Châtillon, France

2. ONERA–The French Aerospace Lab, 92190 Meudon, France

3. Arts and Crafts ParisTech, 75013 Paris, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056100

Reference41 articles.

1. Rotor-vortex interaction noise

2. An experimental investigation of blade-vortex interaction at normal incidence

3. CaryC. M. “An Experimental Investigation of the Chopping of Helicopter Main Rotor Tip Vortices by the Tail Rotor, Part 2: High Speed Photographic Study,” NASA TR 177457, 1987.

4. Contributions to the theory of sound production by vortex-airfoil interaction, with application to vortices with finite axial velocity defect

5. On unsteady surface forces, and sound produced by the normal chopping of a rectilinear vortex

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