Wing Configuration Design
Wing Configuration Design is a methodological framework within aircraft configuration design that specifically governs the determination of geometric, aerodynamic, and structural parameters of a wing to achieve optimal performance, stability, and integration with the overall aircraft architecture.
135
Publications
4.5K
Citations
388
Authors
128
Institutions
Publications per year
2017–2026
36
135
Nobuyuki Umetani, Yuki Koyama, Ryan Schmidt et al. · ACM Transactions on Graphics · 2014 · 119 citations
Design and Wind-Tunnel Analysis of a Fully Adaptive Aircraft Configuration
David A. Neal, Matthew G. Good, Christopher O. Johnston et al. · 2004 · 95 citations
1–5 of 135
388
3
h-index
3
h-index
3
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
3 publications · 95 citations
3
h-index
3
h-index
1–5 of 388
128

Langley Research Center
Hampton, United States
10 h-index
18 publications
1.9K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
7 h-index
20 publications
561 citations
Virginia Tech
Blacksburg, United States
6 h-index
25 publications
1.3K citations
Georgia Institute of Technology
Atlanta, United States
6 h-index
16 publications
307 citations

Beihang University
Beijing, China
4 h-index
13 publications
166 citations
Boeing (Australia)
Brisbane, Australia
3 h-index
5 publications
1.7K citations
Cranfield University
Cranfield, United Kingdom
3 h-index
7 publications
352 citations

Boeing (United States)
Chicago, United States
3 h-index
5 publications
840 citations
1–8 of 128
15 publications · 453 citations
13
h-index
6 publications · 168 citations
6
h-index
AST · 6 publications · 172 citations
6
h-index
Repository · 4 publications · 101 citations
4
h-index
Conference · 3 publications · 54 citations
3
h-index
1–5