Vortex Model and Blade Span Influence on Orthogonal Blade-Vortex Interaction Noise-Reference-Cited by-同舟云学术

Vortex Model and Blade Span Influence on Orthogonal Blade-Vortex Interaction Noise

Published:2020-08 Issue:8 Volume:58 Page:3405-3413
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zehner Paul¹,Falissard Fabrice²,Gloerfelt Xavier³

Affiliation:

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

2. ONERA–The French Aerospace Lab, F-92120 Meudon, France

3. Arts et Métiers ParisTech, Dynfluid Laboratory, F-75013 Paris, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference36 articles.

1. Noise of a model counterrotation propeller with reduced aft rotor diameter at simulated takeoff/approach conditions (F7/A3)

2. Helicopter tail rotor orthogonal blade vortex interaction

3. PeggR.SchidlerP. “Exploratory Wind Tunnel Investigations of the Effect of Main Rotor Wake on Tail Rotor,” NASA CP-2052, 1987.

4. Rotor-vortex interaction noise

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

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