Tip Vortex Reduction
Tip Vortex Reduction is a methodological construct in propeller design that specifically addresses the mitigation of vortical flow structures generated at blade tips by altering blade geometry or flow conditions to minimize energy loss and improve hydrodynamic or aerodynamic efficiency.
99
Publications
2.9K
Citations
260
Authors
103
Institutions
Publications per year
2017–2026
36
Parents
99
Hyun Sik Yoon, D. F. Hill, S. Balachandar et al. · Chemical Engineering Science · 2005 · 93 citations · Full text
Natural Sciences, Mechanical Engineering, Computational Fluid Dynamics +16
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Pennsylvania State University
State College, United States
8 h-index
11 publications
469 citations

Peking University
Beijing, China
7 h-index
12 publications
412 citations
Tsinghua University
Beijing, China
5 h-index
15 publications
687 citations

Harbin Engineering University
Harbin, China
4 h-index
15 publications
332 citations

Glenn Research Center
Cleveland, United States
4 h-index
6 publications
107 citations

Northwestern Polytechnical University
Xi'an, China
4 h-index
17 publications
265 citations

Johns Hopkins University
Baltimore, United States
4 h-index
16 publications
255 citations

Langley Research Center
Hampton, United States
3 h-index
3 publications
96 citations
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7 publications · 304 citations
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6 publications · 229 citations
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5 publications · 232 citations
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5 publications · 156 citations
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AST · 5 publications · 232 citations
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