Shock Train Dynamics
Shock Train Dynamics is a theoretical construct in scramjet propulsion that characterizes the unsteady behavior and spatial evolution of a series of oblique shock waves formed in a supersonic flow, distinguished by its focus on the interaction, propagation, and stabilization mechanisms of shock trains within confined geometries such as isolators.
417
Publications
16.8K
Citations
1.1K
Authors
338
Institutions
Publications per year
2017–2026
148
417
Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow
Justin L. Wagner, Kemal Yuceil, Agustin Valdivia et al. · AIAA Journal · 2009 · 334 citations
A study of the free-piston shock tunnel.
R. J. Stalker · AIAA Journal · 1967 · 228 citations
1–5 of 417
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338

Harbin Institute of Technology
Harbin, China
21 h-index
141 publications
4.9K citations

National University of Defense Technology
Changsha, China
17 h-index
86 publications
2.8K citations
Heilongjiang Institute of Technology
Harbin, China
15 h-index
85 publications
3.3K citations
Taitech (United States)
Beavercreek, United States
15 h-index
22 publications
1.1K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
14 h-index
41 publications
1.5K citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
12 h-index
49 publications
2K citations
University of Michigan
Ann Arbor, United States
11 h-index
28 publications
1.6K citations

Chinese Academy of Sciences
Beijing, China
9 h-index
29 publications
834 citations
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36 publications · 2.2K citations
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31 publications · 1.7K citations
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AST · 27 publications · 1.1K citations
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20 publications · 919 citations
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23 publications · 803 citations
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