Extensible Rectangular Nozzle Model System-Reference-Cited by-同舟云学术

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Extensible Rectangular Nozzle Model System

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Frate Franco¹,Bridges James²

Affiliation:

1. ASRC Aerospace Corporation

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-975

Reference36 articles.

1. Seiner,J.M.andKrejsa,E.A."SupersonicJetNoiseandtheHighSpeedCivilTransport",AIAAPaper,1989-2358, 1989.

2. Zaman,K.B.M.Q."SpreadingCharacteristicsandThrustofJetsfromAsymmetricNozzles",AIAAPaper96-0200, 1996.

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2. Localization of Single and Multi-Stream, Rectangular, Supersonic Jet Noise Sources;AIAA SCITECH 2024 Forum;2024-01-04

3. Nozzle Length and Aft Deck Effects on the Aeroacoustics of Dual Stream Supersonic Jets;AIAA Scitech 2020 Forum;2020-01-05

4. Nozzle Configuration Effects on the Aeroacoustics of Dual Stream Supersonic Jets;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18

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