Composite Fuselage Design
Composite Fuselage Design is a structural engineering methodology within aerospace design that specifically employs fiber-reinforced polymer composite materials to achieve lightweight, high-strength airframe configurations through integrated material and structural optimization distinct from conventional metallic fuselage construction.
44
Publications
1.5K
Citations
116
Authors
40
Institutions
Publications per year
2017–2026
6
Parents
44
Design and Manufacturing of Tow-Steered Composite Shells Using Fiber Placement
Keyu Wu, Brian Tatting, Brett Smith et al. · 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference · 2009 · 64 citations · Full text
Engineering, Aerospace Engineering, Manufacturing Engineering +17
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Lockheed Martin (United States)
Bethesda, United States
4 h-index
7 publications
330 citations

Boeing (United States)
Chicago, United States
4 h-index
6 publications
212 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
4 h-index
8 publications
148 citations
Georgia Institute of Technology
Atlanta, United States
3 h-index
6 publications
287 citations

Langley Research Center
Hampton, United States
3 h-index
4 publications
132 citations

DEVCOM Army Research Laboratory
Adelphi, United States
3 h-index
5 publications
172 citations
Virginia Tech
Blacksburg, United States
3 h-index
5 publications
160 citations
Missouri University of Science and Technology
Rolla, United States
2 h-index
2 publications
43 citations
1–8 of 40
4 publications · 167 citations
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Repository · 3 publications · 57 citations
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2 publications · 35 citations
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2 publications · 27 citations
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Conference · 1 publications · 64 citations
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