Jet-Noise Reduction by Impinging Microjets: an Acoustic Investigation Testing Microjet Parameters-Reference-Cited by-同舟云学术

Jet-Noise Reduction by Impinging Microjets: an Acoustic Investigation Testing Microjet Parameters

Published:2008-05 Issue:5 Volume:46 Page:1081-1087
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Castelain T.¹,Sunyach M.¹,Juvé D.¹,Béra J.-C.²

Affiliation:

1. Ecole Centrale de Lyon, 69134 Ecully, France

2. Université Claude Bernard Lyon I, 69008 Lyon, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.29411

Reference15 articles.

1. Tam, C. K. W., Aeroacoustics of Flight Vehicles, Theory and Practice, Vol.1, Chap. "Jet Noise Generated by Large-Scale Coherent Motion,"H. H. Hubbard, 1995, pp.311-390.

2. Aeroacoustic Characterization, Noise Reduction, and Dimensional Scaling Effects of High Subsonic Jets

3. Far-Field Acoustic Investigation into Chevron Nozzle Mechanisms and Trends

4. Acoustics and Thrust of Quiet Separate-Flow High-Bypass-Ratio Nozzles

5. Design, fabrication, and testing of a SMA hybrid composite jet engine chevron

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