Unstart Phenomena
Unstart Phenomena is a transient aerodynamic instability in scramjet propulsion systems characterized by the sudden detachment and upstream propagation of a shock train caused by adverse pressure gradients, leading to the collapse of supersonic airflow within the combustor and a subsequent loss of thrust generation.
69
Publications
3.3K
Citations
173
Authors
54
Institutions
Publications per year
2017–2026
13
Variants
Inlet Unstart
69
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
1–5 of 69
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University of Illinois Urbana-Champaign, United States
5 publications · 231 citations
5
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5
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1–5 of 173
54
The University of Texas at Austin
Austin, United States
9 h-index
33 publications
2.9K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
7 h-index
12 publications
285 citations

Harbin Institute of Technology
Harbin, China
6 h-index
27 publications
2K citations

National University of Defense Technology
Changsha, China
4 h-index
18 publications
582 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
4 h-index
14 publications
752 citations

University of Notre Dame
Notre Dame, United States
4 h-index
8 publications
594 citations
Heilongjiang Institute of Technology
Harbin, China
4 h-index
19 publications
1.8K citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
3 h-index
12 publications
854 citations
1–8 of 54
12 publications · 559 citations
11
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7 publications · 792 citations
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AST · 5 publications · 176 citations
5
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3 publications · 120 citations
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3 publications · 132 citations
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