Numerical study on the ring-like vortex structure generated by MVG in high-speed flows with different Mach numbers
Author:
Funder
National Science Foundation
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,General Engineering
Link
https://link.springer.com/content/pdf/10.1007/s13160-021-00484-w.pdf
Reference21 articles.
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3. Dussauge, J.P., Dupont, P., Debieve, J.F.: Unsteadiness in shock wave boundary layer interaction with separation. Aerosp. Sci. Technol. 10(2), 85–91 (2006)
4. Estruch-Samper, D., Vanstone, L., Hillier, R., Ganapathisubramani, B.: Micro vortex generator control of axisymmetric high-speed laminar boundary layer separation. Shock Waves 25(5), 521–533 (2015)
5. Babinsky, H., Li, Y., Ford, C.W.P.: Microramp control of supersonic oblique shock-wave/boundary-layer interactions. AIAA J. 47(3), 668–675 (2009)
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