Computational Studies Supporting Concepts for Supersonic Jet Noise Reduction-Reference-Cited by-同舟云学术

Computational Studies Supporting Concepts for Supersonic Jet Noise Reduction

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Kenzakowski Donald¹,Kannepalli Chandrasekhar¹,Brinckman K.²

Affiliation:

1. Combustion Research and Flow Technology Inc.

2. Combustion Research & Flow Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-518

Reference27 articles.

1. High Speed Jet Noise Reduction Using Microjets

2. CFD Support for Jet Noise Reduction Concept Design and Evaluation for F/A 18 E/F Aircraft

3. Seiner, J.M., Ukeiley, L., and Jansen, B.J. "Application of Chevrons, Centerbody Water Injection, and Inner Divergent Flap Corrugations: FinalReport,"ONRBAA01-016, NCPA/U Miss, February 2003.

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