T-Tail Configuration is an empennage design in which the horizontal stabilizer is mounted at the top of the vertical fin, distinguishing it from conventional and cruciform tail configurations by positioning the tailplane in a T-shaped arrangement to enhance aerodynamic efficiency and control effectiveness at high angles of attack.
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254
Citations
21
Authors
11
Institutions
Publications per year
2017–2026
2
Variants
T-tail
Parents
Publications
6
Aerodynamic design features of the DC-9.
R. S. Shevell, Roger Schaufele · Journal of Aircraft · 1966 · 28 citations
Low-speed wind tunnel test results of the Canard Rotor/Wing concept
Steven Bass, T. W. Thompson, John W. Rutherford et al. · 1993 · 16 citations
Engineering, Aerospace Engineering, Mechanical Engineering +15
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Authors
21
- RP
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- SM
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- MS
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- SS
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- FK
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1–5 of 21
Institutions
11
Vantage Power (United Kingdom)
London, United Kingdom
1 h-index
1 publications
16 citations
Glenn Research Center
Cleveland, United States
1 h-index
1 publications
16 citations
Langley Research Center
Hampton, United States
1 h-index
2 publications
32 citations
Bombardier (Canada)
Montreal, Canada
1 h-index
3 publications
123 citations
Unisys (United States)
Blue Bell, United States
1 h-index
2 publications
32 citations
University of Illinois Urbana-Champaign
Urbana, United States
1 h-index
3 publications
399 citations
Ames Research Center
Mountain View, United States
1 h-index
1 publications
16 citations
Imperial College London
London, United Kingdom
1 h-index
2 publications
40 citations
1–8 of 11
Venues
- Journal of Aircraft
2 publications · 69 citations
2
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- AIAA Journal
1 publications · 20 citations
1
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- Biopolymers
1 publications · 133 citations
1
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- Drone Systems and Applications
1 publications · 10 citations
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