Propeller Stall is a fluid dynamic phenomenon characterized by the separation of airflow from the blade surface of a rotating propeller, resulting in a sudden reduction in thrust generation due to excessive blade angle of attack beyond the critical stall threshold.
4
Publications
194
Citations
9
Authors
4
Institutions
Publications per year
2017–2026
4
Parents
Publications
4
1–5 of 4
Authors
9
- AF
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- CD
1
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- SS
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- JR
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- GD
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1–5 of 9
Institutions
4
Abu Dhabi University
Abu Dhabi, United Arab Emirates
1 h-index
2 publications
40 citations
Université Laval
Québec, Canada
1 h-index
3 publications
96 citations
University of Michigan
Ann Arbor, United States
1 h-index
2 publications
258 citations
Northwestern Polytechnical University
Xi'an, China
1 h-index
2 publications
26 citations
Continuum Dynamics (United States)
Ewing, United States
1 publications
10 citations
1–5 of 4
Venues
- Journal of Fluids Engineering
1 publications · 32 citations
1
h-index
- Journal of Aircraft
1 publications · 129 citations
1
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- Journal of Applied Fluid Mechanics
JAFM · 1 publications · 20 citations
1
h-index
- Aerospace Science and Technology
AST · 1 publications · 13 citations
1
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- IEEE Journal of Oceanic Engineering
1 publications · 10 citations
1–5