Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-epsilon turbulence model-Reference-Cited by-同舟云学术

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Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-epsilon turbulence model

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

KHAVARAN A.¹,KREJSA E.²,KIM C.²

Affiliation:

1. NASA, Lewis Research Center; Sverdrup Technology, Inc., Cleveland, OH

2. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-500

Reference21 articles.

1. Yamamoto, K. J., etal, "Experimental Investigation of Shock-Cell Noise Reduction for Single Stream Nozzles in Simulated Flight - Comprehensive Data Report," NASA CR-168234,1984.

2. Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model

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