Canard-tail Interaction
Canard-Tail Interaction is a fluid-dynamic phenomenon in aerodynamics wherein the wake vortices and downwash originating from a forward-mounted canard surface induce unsteady aerodynamic loads and alter the effective angle of attack on a downstream horizontal tail, thereby influencing the stability, control, and trim characteristics of the aircraft configuration.
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2017–2026
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DEVCOM Army Research Laboratory
Adelphi, United States
1 h-index
2 publications
52 citations
Politecnico di Milano
Milan, Italy
1 h-index
1 publications
95 citations
Centre Inria d'Université Côte d'Azur
Valbonne, France
1 h-index
2 publications
90 citations

University of Plymouth
Plymouth, United Kingdom
1 h-index
1 publications
45 citations
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1 publications · 26 citations
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1 publications · 95 citations
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1 publications · 20 citations
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1 publications · 45 citations
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