Sliding-Plug Approach for Inlet Self-Starting Ability Test in Shock Tunnel
Author:
Affiliation:
1. University of Science and Technology of China, 230027 Hefei, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056723
Reference26 articles.
1. Starting characteristics of supersonic inlets
2. Recent research progress on unstart mechanism, detection and control of hypersonic inlet
3. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking
4. Effects of boundary-layers bleeding on unstart/restart characteristics of hypersonic inlets
5. Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet
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