Intake Unstart
Intake Unstart is a disruptive aerothermodynamic phenomenon in ramjet engines wherein the supersonic diffusing flow within the inlet abruptly transitions to subsonic conditions due to excessive pressure disturbance, causing a breakdown of engine operability and sustained combustion.
14
Publications
691
Citations
35
Authors
15
Institutions
Publications per year
2017–2026
4
Variants
Inlet Unstart
Parents
14
1–5 of 14
35
2
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2
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2
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2
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2
h-index
1–5 of 35
15
Defence Research and Development Laboratory
Hyderabad, India
3 h-index
8 publications
454 citations

Boeing (United States)
Chicago, United States
2 h-index
4 publications
226 citations

Indian Institute of Science Bangalore
Bengaluru, India
2 h-index
9 publications
527 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
1 h-index
2 publications
274 citations
Toronto Metropolitan University
Toronto, Canada
1 h-index
1 publications
28 citations
Stanford University
Stanford, United States
1 h-index
4 publications
424 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
1 h-index
2 publications
76 citations
Korea Advanced Institute of Science and Technology
Daejeon, South Korea
1 h-index
3 publications
51 citations
1–8 of 15
4 publications · 224 citations
4
h-index
2 publications · 140 citations
2
h-index
AST · 2 publications · 72 citations
2
h-index
1 publications · 71 citations
1
h-index
1 publications · 11 citations
1
h-index
1–5