Supersonic Mixing
Supersonic Mixing is a fluid dynamic process in scramjet propulsion systems wherein fuel and oxidizer streams intermingle at supersonic velocities, distinguished from subsonic mixing by the persistence of shock waves and compressibility effects that govern the mixing efficiency and combustion initiation in high-speed airflow.
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2017–2026
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Applications of shock-induced mixing to supersonic combustion
Joseph Yang, TOSHI KUBOTA, E. E. Zukoski · AIAA Journal · 1993 · 348 citations
Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream
Mark Gruber, A. S. Nejad, T. H. Chen et al. · Journal of Propulsion and Power · 1995 · 323 citations
Mixing Enhancement in Supersonic Free Shear Flows
Ephraim Gutmark, K. SCHADOW, Ken Yu · Annual Review of Fluid Mechanics · 1995 · 322 citations
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Babol Noshirvani University of Technology, Iran
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National University of Defense Technology
Changsha, China
30 h-index
259 publications
10.5K citations

Langley Research Center
Hampton, United States
25 h-index
69 publications
2.6K citations

Babol Noshirvani University of Technology
Babol, Iran
19 h-index
23 publications
2.6K citations
Stanford University
Stanford, United States
16 h-index
48 publications
2.9K citations

Khazar University
Baku, Azerbaijan
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15 publications
1.5K citations
Virginia Tech
Blacksburg, United States
15 h-index
30 publications
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Indian Institute of Technology Kanpur
Kanpur, India
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27 publications
683 citations
California Institute of Technology
Pasadena, United States
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21 publications
2.5K citations
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