Stall Onset
Stall Onset is a fluid dynamics phenomenon characterized as the critical condition within aerodynamic lift generation at which airflow separation over an airfoil's upper surface begins, precipitating a nonlinear reduction in lift coefficient and marking the upper limit of attached, streamlined flow prior to full stall.
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5.4K
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114
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2017–2026
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Criteria for Spike Initiated Rotating Stall
Huu Duc Vo, C. S. Tan, E. M. Greitzer · Journal of Turbomachinery · 2008 · 496 citations
Stall Inception in Axial Flow Compressors
I. J. Day · Journal of Turbomachinery · 1993 · 492 citations
Stall Inception in Axial Compressors
N. M. McDougall, N. A. Cumpsty, T. P. Hynes · Journal of Turbomachinery · 1990 · 348 citations
The onset of dynamic stall revisited
Karen Mülleners, Markus Raffel · Experiments in Fluids · 2011 · 260 citations · Full text
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University of Cambridge
Cambridge, United Kingdom
10 h-index
22 publications
3K citations

University of Glasgow
Glasgow, United Kingdom
7 h-index
19 publications
1.1K citations

Beihang University
Beijing, China
6 h-index
16 publications
474 citations
Massachusetts Institute of Technology
Cambridge, United States
6 h-index
14 publications
1.7K citations

Naval Postgraduate School
Monterey, United States
5 h-index
6 publications
124 citations

Ames Research Center
Mountain View, United States
4 h-index
4 publications
117 citations
Sainsbury Laboratory
Norwich, United Kingdom
4 h-index
8 publications
1.9K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
3 h-index
9 publications
667 citations
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17 publications · 2.2K citations
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9 publications · 313 citations
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7 publications · 223 citations
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Conference · 5 publications · 99 citations
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