Angle Of Attack Effects
Angle of Attack Effects is a theoretical construct in aerodynamics that denotes the causal relationship between the angle formed by the chord line of an airfoil and the relative wind direction, and the resulting aerodynamic forces and moments, particularly lift and flow separation characteristics, which determine stall onset and post-stall behavior.
350
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10.7K
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816
Authors
271
Institutions
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2017–2026
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Langley Research Center
Hampton, United States
21 h-index
63 publications
2.1K citations

Ames Research Center
Mountain View, United States
16 h-index
29 publications
1.2K citations
Technion – Israel Institute of Technology
Haifa, Israel
9 h-index
15 publications
362 citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
8 h-index
11 publications
224 citations
Virginia Tech
Blacksburg, United States
7 h-index
14 publications
365 citations

University of Notre Dame
Notre Dame, United States
7 h-index
10 publications
343 citations

Armstrong Flight Research Center
Edwards, United States
6 h-index
9 publications
183 citations
Georgia Institute of Technology
Atlanta, United States
6 h-index
12 publications
209 citations
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45 publications · 1.4K citations
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Repository · 21 publications · 482 citations
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Repository · 12 publications · 334 citations
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Repository · 14 publications · 265 citations
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