Rocket Combustion Instability
Rocket Combustion Instability is a combustion instability phenomenon characterized by self-sustained, large-amplitude pressure oscillations occurring within the combustion chamber of a rocket engine, arising from detrimental coupling between unsteady heat release and acoustic modes of the system.
250
Publications
9.8K
Citations
444
Authors
139
Institutions
Publications per year
2017–2026
46
Variants
Combustion Instability In Rocket Engines
Parents
250
1–5 of 250
444
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
13 publications · 425 citations
13
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13
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13
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
12 publications · 378 citations
12
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10
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1–5 of 444
139
Purdue University West Lafayette
West Lafayette, United States
16 h-index
74 publications
2.9K citations
Naval Air Warfare Center Weapons Division
China Lake Acres, United States
13 h-index
28 publications
1.4K citations
Princeton University
Princeton, United States
11 h-index
18 publications
1.3K citations
University of Tennessee at Knoxville
Knoxville, United States
10 h-index
20 publications
1K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
9 h-index
29 publications
1K citations
Edwards Air Force Base
Edwards Air Force Base, United States
9 h-index
17 publications
846 citations
Georgia Institute of Technology
Atlanta, United States
8 h-index
17 publications
778 citations
University of California, Irvine
Irvine, United States
8 h-index
25 publications
776 citations
1–8 of 139
54 publications · 2.5K citations
28
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36 publications · 1.4K citations
21
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10 publications · 507 citations
10
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9 publications · 286 citations
9
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Repository · 7 publications · 657 citations
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