Control Surface Effects
Control Surface Effects is the body of aerodynamic and flight-dynamic phenomena by which deflections of an aircraft’s control surfaces modify the distribution of aerodynamic forces and moments, thereby altering its attitude, response, stability, and control characteristics.
207
Publications
10.1K
Citations
511
Authors
171
Institutions
Publications per year
2017–2026
34
Parents
Children
Adverse YawAerodynamic Balance Of Control SurfacesAileron EffectivenessAileron ReversalBoundary Layer Control On Control SurfacesControl Surface Aerodynamic DampingControl Surface Authority At High Angle Of AttackControl Surface Coupling EffectsControl Surface Deflection EffectsControl Surface Drag Rise
207
1–5 of 207
511
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United States Air Force Research Laboratory, United States
4 publications · 129 citations
4
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3
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1–5 of 511
171

Langley Research Center
Hampton, United States
13 h-index
27 publications
796 citations

Ames Research Center
Mountain View, United States
9 h-index
13 publications
708 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
6 h-index
12 publications
282 citations
Duke University
Durham, United States
6 h-index
20 publications
1.9K citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
6 h-index
10 publications
351 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
6 h-index
10 publications
142 citations

Delft University of Technology
Delft, The Netherlands
4 h-index
11 publications
363 citations
Virginia Tech
Blacksburg, United States
4 h-index
21 publications
1.1K citations
1–8 of 171
29 publications · 789 citations
18
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AST · 11 publications · 258 citations
10
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9 publications · 297 citations
9
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5 publications · 582 citations
5
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5 publications · 210 citations
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1–5