Wing Structural Optimization
Wing Structural Optimization is a computational and analytical methodology within aerospace engineering that systematically refines the material distribution, component sizing, and load-carrying architecture of wing structures to achieve optimal performance metrics—such as weight reduction, strength enhancement, or stiffness maximization—under prescribed constraints and design criteria.
141
Publications
5.1K
Citations
355
Authors
134
Institutions
Publications per year
2017–2026
43
Parents
141
Seung Ki Moon, Yu En Tan, Jihong Hwang et al. · International Journal of Precision Engineering and Manufacturing-Green Technology · 2014 · 286 citations · Full text
Engineering, Aerospace Engineering, Materials Engineering +14
1–5 of 141
355
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134
Virginia Tech
Blacksburg, United States
14 h-index
59 publications
2.3K citations
University of Florida
Gainesville, United States
10 h-index
18 publications
766 citations

Langley Research Center
Hampton, United States
8 h-index
12 publications
555 citations

Delft University of Technology
Delft, The Netherlands
7 h-index
14 publications
302 citations
University of Michigan
Ann Arbor, United States
7 h-index
13 publications
756 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
5 h-index
7 publications
273 citations
Georgia Institute of Technology
Atlanta, United States
5 h-index
8 publications
286 citations
Cranfield University
Cranfield, United Kingdom
4 h-index
5 publications
231 citations
1–8 of 134
12 publications · 784 citations
11
h-index
10 publications · 406 citations
10
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AST · 9 publications · 501 citations
9
h-index
8 publications · 310 citations
8
h-index
4 publications · 152 citations
4
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