Topological Geometry Interpretation of Supersonic Inlet Start/Unstart Based on Catastrophe Theory
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Heilongjiang, People ’ s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34125
Reference13 articles.
1. Prediction of supersonic inlet unstart caused by freestream disturbances
2. Boundary conditions for unsteady supersonic inlet analyses
3. High-speed inlet unstart calculations using an implicit solution adaptive mesh algorithm
4. Investigations of High-Speed Civil Transport Inlet Unstart at Angle of Attack
5. Numerical Simulation of High-Speed Civil Transport Inlet Operability with Angle of Attack
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