Large-Eddy Simulations of a Supersonic Jet and Its Near-Field Acoustic Properties-Reference-Cited by-同舟云学术

Large-Eddy Simulations of a Supersonic Jet and Its Near-Field Acoustic Properties

Published:2009-08 Issue:8 Volume:47 Page:1849-1865
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Junhui,Kailasanath K.,Ramamurti Ravi,Munday David,Gutmark Ephraim,Lohner Rainald¹

Affiliation:

1. George Mason University, Fairfax, Virginia 22030

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.43281

Reference35 articles.

1. Shock associated noise of supersonic jets from convergent-divergent nozzles

2. Tam, C. K. W. "Jet Noise Generated by large Scale Coherent Motion, Aeroacoustics of Flight Vehicles: Theory and Practice," Vol.1, edited by H. H. Hubbard,NASA RP-1258,1991, pp.311-390.

3. Supersonic Jet Noise

4. Broadband Shock Noise from Supersonic Jets

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