Isolator Flow Dynamics
Isolator Flow Dynamics is a theoretical framework within hypersonic propulsion engineering that characterizes the behavior of shock-induced boundary layer interactions and pressure disturbances in the isolator section of scramjet engines, distinguishing it from other propulsion flow models by its focus on unsteady flow stabilization and inlet-combustor coupling under hypersonic conditions.
150
Publications
6K
Citations
375
Authors
105
Institutions
Publications per year
2017–2026
69
Parents
150
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
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105

Harbin Institute of Technology
Harbin, China
16 h-index
78 publications
2.6K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
13 h-index
35 publications
1.3K citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
11 h-index
36 publications
1.7K citations
The University of Texas at Austin
Austin, United States
11 h-index
41 publications
3.4K citations
Taitech (United States)
Beavercreek, United States
9 h-index
11 publications
332 citations

Northwestern Polytechnical University
Xi'an, China
9 h-index
27 publications
718 citations
Heilongjiang Institute of Technology
Harbin, China
7 h-index
28 publications
1.1K citations
Sandia National Laboratories
Albuquerque, United States
5 h-index
5 publications
362 citations
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21 publications · 1K citations
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15 publications · 1.1K citations
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9 publications · 476 citations
9
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9 publications · 364 citations
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AST · 8 publications · 205 citations
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