The Kutta Condition is a boundary condition in aerodynamic theory that specifies the circulation around a lifting airfoil such that the flow leaves the trailing edge smoothly, distinguishing it from other potential flow solutions by ensuring physically realistic behavior at the trailing edge.
129
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7.5K
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224
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94
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Publications per year
2017–2026
10
Parents
Publications
129
Lift and the leading-edge vortex
C. W. Pitt Ford, Holger Babinsky · Journal of Fluid Mechanics · 2013 · 231 citations
1–5 of 129
Authors
224
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1–5 of 224
Institutions
94
University of Cambridge
Cambridge, United Kingdom
9 h-index
12 publications
811 citations
Ames Research Center
Mountain View, United States
8 h-index
18 publications
454 citations
Massachusetts Institute of Technology
Cambridge, United States
6 h-index
8 publications
280 citations
University College London
London, United Kingdom
4 h-index
6 publications
188 citations
Langley Research Center
Hampton, United States
4 h-index
6 publications
2.1K citations
University of California, Los Angeles
Los Angeles, United States
3 h-index
4 publications
106 citations
Boeing (United States)
Chicago, United States
3 h-index
7 publications
150 citations
Virginia Tech
Blacksburg, United States
3 h-index
5 publications
261 citations
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Venues
- Journal of Fluid Mechanics
35 publications · 2.3K citations
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- AIAA Journal
13 publications · 685 citations
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- Journal of Aircraft
5 publications · 355 citations
5
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- Journal of Ship Research
5 publications · 97 citations
5
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- The Quarterly Journal of Mechanics and Applied Mathematics
QJMAM · 3 publications · 65 citations
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