Spectral Content in a Supersonic Backward-Facing Step Flow
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
2. Ohio State University, Columbus, Ohio 43210
Funder
Dayton Area Graduate Studies Institute
Air Force Office of Scientific Research
Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34890
Reference44 articles.
1. Supersonic flow over an axisymmetric backward-facing step
2. Effects of Inlet Configuration on Ignition and Fuel Regression Behind a Backstep
3. Effect of Coolant Inlet Conditions on Supersonic Film Cooling
4. A Review of Research on Subsonic Turbulent Flow Reattachment
5. Numerical simulations of laminar flow over a 3D backward-facing step
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