Empennage Configuration
Empennage Configuration is a structural design framework in aerospace engineering that specifies the arrangement and orientation of an aircraft's tail surfaces, distinguishing it from other airframe configurations by its role in providing stability and control about the pitch and yaw axes.
7
Publications
107
Citations
19
Authors
9
Institutions
Publications per year
2017–2026
4
Variants
Tail Configuration
Parents
7
Design and Manufacture of a Solar-Powered Unmanned Aerial Vehicle for Civilian Surveillance Missions
Nelson Javier Pedraza Betancourth, Julio Enoc Parra Villamarín, John Jairo Vaca Ríos et al. · Journal of Aerospace Technology and Management · 2016 · 30 citations · Full text
Engineering, Aerospace Engineering, Manufacturing Engineering +17
1–5 of 7
19
1
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Fundación Universitaria Los Libertadores, Colombia
1 publications · 30 citations
1
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1
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1
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1–5 of 19
9
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
1 h-index
2 publications
32 citations
United States Navy
Washington, United States
1 h-index
2 publications
26 citations
Italian Aerospace Research Centre
Capua, Italy
1 h-index
1 publications
16 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
14 citations

Trinity College Dublin
Dublin, Ireland
1 h-index
2 publications
32 citations

University of Naples Federico II
Naples, Italy
1 h-index
4 publications
44 citations
Airbus (France)
Toulouse, France
1 h-index
1 publications
13 citations
Airbus (Spain)
Getafe, Spain
1 h-index
1 publications
13 citations
1–8 of 9
2 publications · 21 citations
2
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1 publications · 16 citations
1
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1 publications · 13 citations
1
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1 publications · 13 citations
1
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1 publications · 30 citations
1
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1–5