Control Surface Deflection Effects
Control Surface Deflection Effects is a mechanical aerodynamic phenomenon denoting the alterations in aerodynamic forces and moments on an aircraft resulting from the angular displacement of control surfaces relative to the airflow, distinguished by its direct influence on the vehicle's stability and maneuverability.
15
Publications
636
Citations
39
Authors
16
Institutions
Publications per year
2017–2026
2
Parents
15
1–5 of 15
39
2
h-index
2
h-index
1
h-index
Nielsen Engineering & Research (United States), United States
1 publications · 19 citations
1
h-index
United States Air Force Research Laboratory, United States
1 publications · 26 citations
1
h-index
1–5 of 39
16

Centre National de la Recherche Scientifique
Paris, France
2 h-index
4 publications
322 citations

Ames Research Center
Mountain View, United States
2 h-index
6 publications
474 citations

Indian Institute of Technology Kanpur
Kanpur, India
1 h-index
2 publications
26 citations
Honam University
Gwangju, South Korea
1 h-index
1 publications
12 citations

Langley Research Center
Hampton, United States
1 h-index
3 publications
33 citations
Universidade de São Paulo
São Paulo, Brazil
1 h-index
2 publications
120 citations
Technion – Israel Institute of Technology
Haifa, Israel
1 h-index
1 publications
13 citations
University of California, Davis
Davis, United States
1 h-index
1 publications
141 citations
1–8 of 16
4 publications · 105 citations
4
h-index
2 publications · 161 citations
2
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1 publications · 67 citations
1
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1 publications · 17 citations
1
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Conference · 1 publications · 26 citations
1
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