Bypass Ratio is a dimensionless performance metric in turbofan engine design that quantifies the ratio of the mass flow rate of air bypassing the engine core to the mass flow rate passing through the core.
193
Publications
5.2K
Citations
448
Authors
125
Institutions
Publications per year
2017–2026
41
Parents
Publications
193
1–5 of 193
Authors
448
- DP
10
h-index
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7
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7
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7
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6
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1–5 of 448
Institutions
125
Glenn Research Center
Cleveland, United States
17 h-index
40 publications
1.4K citations
Langley Research Center
Hampton, United States
16 h-index
38 publications
1.1K citations
Cranfield University
Cranfield, United Kingdom
14 h-index
55 publications
1.4K citations
Rolls-Royce (United Kingdom)
London, United Kingdom
13 h-index
25 publications
567 citations
University of California, Irvine
Irvine, United States
9 h-index
17 publications
404 citations
MTU Aero Engines (Germany)
Munich, Germany
8 h-index
14 publications
416 citations
University of Cambridge
Cambridge, United Kingdom
8 h-index
20 publications
383 citations
Boeing (United States)
Chicago, United States
7 h-index
11 publications
294 citations
1–8 of 125
Venues
- Journal of Propulsion and Power
15 publications · 422 citations
13
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- Journal of Turbomachinery
10 publications · 188 citations
10
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- AIAA Journal
8 publications · 418 citations
8
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- NASA Technical Reports Server (NASA)
Repository · 7 publications · 150 citations
7
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- NASA STI Repository (National Aeronautics and Space Administration)
Repository · 6 publications · 125 citations
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