Bistability and Hysteresis in a Nonlinear Dynamic Model of Shock Motion
Author:
Affiliation:
1. School of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China
2. College of Engineering, Peking University, 100871 Peking, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032175
Reference14 articles.
1. SusumuM.KeiichiK. “Unstart Phenomenon Due to Thermal Choke in Scramjet Module,” AIAA paper 2001-1887, 2001.
2. Prediction of supersonic inlet unstart caused by freestream disturbances
3. Design of a Near-Isentropic Supersonic Inlet Using Active Control
4. KantrowitzA. “The Formation and Stability of Normal Shock Waves in Channel Flows,” NACA TN-1225, 1947.
5. HurrellH. G. “Analysis of Shock Motion in Ducts During Disturbances in Downstream Pressure,” NACA TN-4090, 1957.
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