Experimental/Numerical Study of Ducted-Fan Noise: Effect of Duct Inlet Shape-Reference-Cited by-同舟云学术

Experimental/Numerical Study of Ducted-Fan Noise: Effect of Duct Inlet Shape

Published:2018-03 Issue:3 Volume:56 Page:979-996
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Shur Michael,Strelets Michael,Travin Andrey,Christophe Julien,Kucukcoskun Korcan,Schram Christophe,Sack Stefan,Åbom Mats

Funder

European Commission FP7 Collaborative Project IDEALVENT

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055870

Reference40 articles.

1. Spectrum of rotor noise caused by atmospheric turbulence

2. Effects of Ingested Atmospheric Turbulence on Measured Tail Rotor Acoustics

3. LakshminarayanaB.MiseevN.ThompsonD. E. “Noise due to Interaction of Inlet Turbulence and Guide Vane Secondary Flow with Propulsor,” Pennsylvania State Univ. TM 75-237, State College, PA, Oct. 1975.

4. Inlet Flow Conditions and Tonal Sound Radiation from a Subsonic Fan

5. Effects of Inflow Distortion Profiles on Fan Tone Noise

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