Canard Configuration is an aircraft configuration design in which a small forewing or foreplane is positioned forward of the main wings to provide pitch control and enhance aerodynamic performance, distinguishing it from conventional tail-aft configurations.
85
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1.9K
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181
Authors
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Publications per year
2017–2026
10
Variants
Canard Design
Publications
85
Rapid airplane parametric input design (RAPID)
Robert E. Smith, M. Susan Bloor, Michael J. Wilson et al. · 1995 · 64 citations
Engineering, Aerospace Engineering, Computational Engineering +17
John Guckenheimer, Radu Haiduc · Moscow Mathematical Journal · 2005 · 58 citations
Aerodynamics of Strake-Wing Interactions
James M. Luckring · Journal of Aircraft · 1979 · 44 citations
1–5 of 85
Authors
181
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1–5 of 181
Institutions
84
Langley Research Center
Hampton, United States
11 h-index
16 publications
359 citations
United States Army
Arlington, United States
5 h-index
10 publications
290 citations
Technion – Israel Institute of Technology
Haifa, Israel
4 h-index
8 publications
182 citations
Beihang University
Beijing, China
4 h-index
17 publications
387 citations
U.S. Army Aviation and Missile Command
Huntsville, United States
4 h-index
8 publications
222 citations
Ames Research Center
Mountain View, United States
4 h-index
4 publications
74 citations
DEVCOM Army Research Laboratory
Adelphi, United States
4 h-index
5 publications
171 citations
Technische Universität Braunschweig
Braunschweig, Germany
3 h-index
6 publications
114 citations
1–8 of 84
Venues
- Journal of Aircraft
28 publications · 569 citations
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- NASA STI Repository (National Aeronautics and Space Administration)
Repository · 5 publications · 108 citations
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- Journal of Spacecraft and Rockets
3 publications · 84 citations
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- Aerospace Science and Technology
AST · 3 publications · 64 citations
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- Aerospace
2 publications · 52 citations
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