Characterization of Turbulent Supersonic Flow over a Backward-Facing Step
Author:
Affiliation:
1. Indian Institute of Technology Kanpur, Kanpur 208 016, India
Funder
IITK-STC
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J054709
Reference46 articles.
1. Numerical solution of the turbulent supersonic flow over a backward facing step
2. ChapmanD. “An Analysis of the Base Pressure at Supersonic Velocities and Comparison with Experiment,” NACA TR 1051, 1951.
3. Supersonic sudden-expansion flow with fluid injection - An experimental and computational study
4. On the separation of a supersonic flow at a sharp corner.
5. Experimental studies on the lip shock.
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