Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction-Reference-Cited by-同舟云学术

Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction

Published:2003-05-12 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/CEAS Aeroacoustics Conference and Exhibit
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Author:

Massey Steven¹,Thomas Russell²,Abdol-Hamid Khaled³,Elmiligui Alaa³

Affiliation:

1. Eagle Aeronautics Inc.

2. NASA Langley Research Center

3. Analytical Services & Materials Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3212

Reference11 articles.

1. 1Early, K. "Propulsion Airframe Integration Design, Analysis and ChallengesGoingIntothe21stCentury,"PaperNo.6103,2000,Presented atthe InternationalCouncil oftheAeronautical Sciences.

2. 2Thomas,R.H.,Kinzie,K.W.,andPao,S.P."ComputationalAnalysis of a Pylon-Chevron Core Nozzle Interaction," AIAA Paper 2001-2185,2001.

3. 3Hunter,C.A.andThomas,R.H."DevelopmentofaJetNoisePredictionMethodforInstalledJetConfigurations,"AIAAPaper2003-3169, 2003.

4. The prediction of laminarization with a two-equation model of turbulence

5. 5Abdol-Hamid, K. S., Pao, S. P., Massey, S. J., and Elmiligui, A. A. "Temperature Corrected Turbulence Model for High Temperature JetFlow,"AIAAPaper2003-4070,2003.

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