Fuselage Composite Structures
Fuselage Composite Structures is a structural engineering construct that refers to the load-bearing airframe configuration of an aircraft's main body, distinguished by its primary construction from fiber-reinforced polymeric or advanced composite materials engineered to optimize strength-to-weight ratios and resist aerodynamic and operational stresses.
104
Publications
3.5K
Citations
326
Authors
90
Institutions
Publications per year
2017–2026
29
Parents
104
The mechanical behavior of GLARE laminates for aircraft structures
Guocai Wu, J.‐M. Yang · JOM · 2005 · 366 citations
Engineering, Aerospace Engineering, Materials Engineering +14
Elena Dilonardo, Michele Nacucchi, Fabio De Pascalis et al. · Composites Science and Technology · 2020 · 93 citations
Engineering, Aerospace Engineering, Materials Engineering +15
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Langley Research Center
Hampton, United States
10 h-index
16 publications
344 citations

Boeing (United States)
Chicago, United States
8 h-index
9 publications
247 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
6 h-index
8 publications
341 citations

Delft University of Technology
Delft, The Netherlands
5 h-index
10 publications
224 citations

University of Campania "Luigi Vanvitelli"
Caserta, Italy
5 h-index
18 publications
657 citations
Italian Aerospace Research Centre
Capua, Italy
5 h-index
11 publications
415 citations

Imperial College London
London, United Kingdom
4 h-index
16 publications
735 citations
Georgia Institute of Technology
Atlanta, United States
4 h-index
10 publications
508 citations
1–8 of 90
4 publications · 229 citations
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5 publications · 169 citations
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Repository · 5 publications · 69 citations
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Repository · 4 publications · 119 citations
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3 publications · 133 citations
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