Significance of shock structure on supersonic jet mixing noise of axisymmetric nozzles
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
2. NYMA, Lewis Research Group, Brook Park, Ohio 44142
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12192
Reference6 articles.
1. On a New Theory of free Turbulence
2. Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-epsilon turbulence model
3. PARC Code: Theory and Usage
4. Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model
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