Tail Structural Loads
Tail Structural Loads is a structural engineering construct that quantifies the distributed forces and moments acting on the tail section of an aerospace vehicle during flight, distinguishing it from other airframe load analyses by focusing specifically on aerodynamic, inertial, and control surface-induced stresses inherent to tail assemblies.
7
Publications
179
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Authors
6
Institutions
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2017–2026
0
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K. Schindler · Space Science Reviews · 1979 · 34 citations
Ideal Tail Load for Minimum Aircraft Drag
E. V. Laitone · Journal of Aircraft · 1978 · 21 citations
Engineering, Aerospace Engineering, Mechanical Engineering +13
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Virginia Tech
Blacksburg, United States
1 h-index
2 publications
42 citations
Ruhr University Bochum
Bochum, Germany
1 h-index
1 publications
34 citations
ITER
Vinon-sur-Verdon, France
1 h-index
7 publications
126 citations

Cornell University
Ithaca, United States
1 h-index
2 publications
96 citations
Assystem (France)
Paris, France
1 h-index
5 publications
90 citations
University of California, Berkeley
Berkeley, United States
1 h-index
1 publications
21 citations
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1 publications · 21 citations
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1 publications · 34 citations
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1 publications · 21 citations
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1 publications · 48 citations
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1 publications · 18 citations
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