Fuselage Weight Optimization
Fuselage Weight Optimization is a systematic engineering methodology aimed at minimizing the structural mass of an aircraft fuselage while maintaining required performance, safety, and design constraints through the integrated application of materials selection, configuration design, and analytical modeling techniques.
8
Publications
227
Citations
29
Authors
6
Institutions
Publications per year
2017–2026
1
Parents
8
1–5 of 8
29
2
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
2 publications · 53 citations
2
h-index
1
h-index
1
h-index
1
h-index
1–5 of 29
6

University of Leeds
Leeds, United Kingdom
1 h-index
3 publications
123 citations
Politecnico di Milano
Milan, Italy
1 h-index
2 publications
24 citations

Langley Research Center
Hampton, United States
1 h-index
8 publications
112 citations
Virginia Tech
Blacksburg, United States
1 h-index
4 publications
108 citations

Technische Universität Darmstadt
Darmstadt, Germany
1 h-index
2 publications
100 citations
Technosoft (United States)
Cincinnati, United States
1 h-index
2 publications
28 citations
1–6 of 6
2 publications · 71 citations
2
h-index
2 publications · 53 citations
2
h-index
1 publications · 50 citations
1
h-index
Repository · 1 publications · 12 citations
1
h-index
1 publications · 27 citations
1
h-index
1–5