Interactive Phenomena in Supersonic Jet Mixing Problems, Part 11: Numerical Studies
Author:
Affiliation:
1. Science Applications, Inc., Princeton, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48580
Reference19 articles.
1. Interactive phenomena in supersonic jet mixing problems. I Phenomenology and numerical modeling techniques
2. Experiments of shock associated noise of supersonic jets
3. Aerodynamic aspects of shock containing jet plumes
4. Shock noise features using the SCIPVIS code
5. Shock-capturing parabolized Navier-Stokes model /SCIPVIS/ for the analysis of turbulent underexpanded jets
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