Acoustic source indicators using LES in a fully expanded and heated supersonic jet-Reference-Cited by-同舟云学术

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Acoustic source indicators using LES in a fully expanded and heated supersonic jet

Published:2013-05-24 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Fiévet Romain¹,Tinney Charles E.¹,Murray Nathan²,Lyons Gregory²,Panickar Praveen³

Affiliation:

1. University of Texas, Austin

2. University of Mississippi, University

3. Combustion Research and Flow Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2193

Reference27 articles.

1. Application of Lighthill's Equation to a Mach 1.92 Turbulent Jet

2. Numerical Simulation of a Mach 1.92 Turbulent Jet and Its Sound Field

3. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9

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1. A proper framework for studying noise from jets with non-compact sources;Journal of Fluid Mechanics;2021-10-27

2. Overview of the Use of Large-Eddy Simulations in Jet Aeroacoustics;AIAA Journal;2020-04

3. Large-Eddy Simulations Analysis of Supersonic Heated Jets with Fluid Injection for Noise Reduction;AIAA Journal;2019-08

4. The Use of Large Eddy Simulations in Jet Aeroacoustics;AIAA Scitech 2019 Forum;2019-01-06

5. Optical Flow Visualization of a Mach 3 jet at 150,000 frames per second;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

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