Investigation of a High-Mach-Number Overexpanded Jet Using Large-Eddy Simulation
Author:
Affiliation:
1. Ecole Centrale de Lyon, 69134 Ecully, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050952
Reference67 articles.
1. Experimental Study and Simulation of Rocket Engine Freejet Noise
2. The Mach wave field radiated by supersonic turbulent shear flows
3. On the three families of instability waves of high-speed jets
4. PREDICTION OF SUPERSONIC JET NOISE FROM A STATISTICAL ACOUSTIC MODEL AND A COMPRESSIBLE TURBULENCE CLOSURE
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