Numerical Simulation of a Mach 1.92 Turbulent Jet and Its Sound Field
Author:
Affiliation:
1. University of California, Los Angeles, Los Angeles, California 90095
2. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.889
Reference26 articles.
1. Supersonic Jet Noise
2. Sound generated by instability waves of supersonic flows. Part 2. Axisymmetric jets
3. The compressible turbulent shear layer: an experimental study
4. The spatial viscous instability of axisymmetric jets
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