Aerothermodynamic characteristics of hypersonic curved compression ramp flows with bistable states
Author:
Affiliation:
1. Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Centre, Mianyang 621000, China
2. China Aerodynamics Research and Development Centre, Mianyang 621000, China
Funder
China Postdoctoral Science Foundation
National Nature Science
CARDC Fundamental and Frontier Technology Research Fund
National Key Research and Development Program of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0069666
Reference57 articles.
1. Experimental, analytical, and computational methods applied to hypersonic compression ramp flows
2. Experimental and computational investigations of hypersonic flow about compression ramps
3. Hypersonic Curved Compression Inlet and Its Inverse Design
4. Bistable states and separation hysteresis in curved compression ramp flows
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