Combustion Induced Choking and Unstart Initiation in a Circular Constant-Area Supersonic Flow
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057921
Reference48 articles.
1. AIAA Education Series;Heiser W. H.,1993
2. Recent research progress on unstart mechanism, detection and control of hypersonic inlet
3. Unstart phenomena induced by flow choking in scramjet inlet-isolators
4. B. One-Dimensional Treatment of Steady Gas Dynamics
5. The Mechanism of Pseudo-Shock Waves
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