On the wake structure of a micro-ramp vortex generator in hypersonic flow
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, Mianyang, Sichuan 621000, China
2. Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, Sichuan 621000, China
Funder
National Key Research and Development Program of China
National Numerical Windtunnel Project
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0030975
Reference31 articles.
1. Hypersonic and High-Temperature Gas Dynamics, Second Edition
2. Review of research on low-profile vortex generators to control boundary-layer separation
3. Microvortex generators in high-speed flow
4. Micro-vortex generators for shock wave/boundary layer interactions
5. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
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