Fuselage Cross-section Design
Fuselage Cross-Section Design is a methodological framework within aerospace engineering that defines the geometric and structural configuration of a fuselage’s transverse section, distinguished by its focus on optimizing aerodynamic efficiency, structural integrity, and internal volume allocation in relation to aircraft performance requirements.
11
Publications
213
Citations
38
Authors
8
Institutions
Publications per year
2017–2026
3
Parents
11
1–5 of 11
38
2
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1–5 of 38
8

University of Pisa
Pisa, Italy
2 h-index
4 publications
78 citations
Civil Aviation University of China
Tianjin, China
1 h-index
5 publications
115 citations
University of Stuttgart
Stuttgart, Germany
1 h-index
1 publications
19 citations
Kawasaki Heavy Industries (Japan)
Tokyo, Japan
1 h-index
6 publications
156 citations
Aalborg University
Aalborg, Denmark
1 h-index
1 publications
18 citations
University of Delaware
Newark, United States
1 h-index
1 publications
18 citations
Missouri University of Science and Technology
Rolla, United States
1 h-index
1 publications
21 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
16 citations
1–8 of 8
1 publications · 12 citations
1
h-index
1 publications · 16 citations
1
h-index
1 publications · 19 citations
1
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1 publications · 21 citations
1
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1 publications · 18 citations
1
h-index
1–5