Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. AVIC Shenyang Aircraft Design and Research Institute, 110035 Shenyang, People’s Republic of China
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061375
Reference37 articles.
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3. Recent research progress on unstart mechanism, detection and control of hypersonic inlet
4. Large-Eddy Simulation of a Supersonic Inlet-Isolator
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