Aeroacoustics of a Planar Multistream Supersonic Nozzle with Aft Deck and Sidewalls-Reference-Cited by-同舟云学术

Aeroacoustics of a Planar Multistream Supersonic Nozzle with Aft Deck and Sidewalls

Published:2018-10 Issue:10 Volume:56 Page:3926-3937
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Tinney Charles E.¹,Panickar Praveen²,Vogel Patrick²

Affiliation:

1. University of Texas at Austin, Austin, Texas 78713

2. Combustion Research and Flow Technology, Inc., Pipersville, Pennsylvania 18947

Funder

The Air Force Research Laboratories

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056735

Reference47 articles.

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2. YetterJ. A.LeavittL. D. “Effects of Sidewall Geometry on the Installed Performance of Nonaxisymmetric Convergent-Divergent Exhaust Nozzles,” NASA TP 1771, Dec. 1980.

3. The nonaxisymmetric nozzle - It is for real<149>fighter aircraft performance viewpoint

4. On the Noise Emanating from a Two-Dimensional Jet Above the Critical Pressure

5. The role of screech tones in mixing of an underexpanded rectangular jet

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