Fuselage Deformation Analysis
Fuselage Deformation Analysis is a computational and experimental methodology within aerospace structural engineering that specifically characterizes the spatial and temporal changes in fuselage geometry under operational loads, distinguishing itself by its focus on strain distribution, buckling behavior, and elasticity in thin-walled aircraft pressure cabins.
17
Publications
457
Citations
47
Authors
24
Institutions
Publications per year
2017–2026
6
Parents
17
1–5 of 17
47
1
h-index
1
h-index
1
h-index
Sikorsky Aircraft Corporation (United States), United States
1 publications · 10 citations
1
h-index
1
h-index
1–5 of 47
24
University of Delaware
Newark, United States
1 h-index
1 publications
11 citations
University of Minho
Braga, Portugal
1 h-index
1 publications
23 citations

University of Campania "Luigi Vanvitelli"
Caserta, Italy
1 h-index
4 publications
172 citations
Kremenchuk Mykhailo Ostrohradskyi National University
Kremenchuk, Ukraine
1 h-index
1 publications
29 citations
Sikorsky Aircraft Corporation (United States)
Huntsville, United States
1 h-index
1 publications
10 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
10 citations
Aalborg University
Aalborg, Denmark
1 h-index
1 publications
11 citations
Italian Aerospace Research Centre
Capua, Italy
1 h-index
2 publications
86 citations
1–8 of 24
2 publications · 23 citations
2
h-index
1 publications · 29 citations
1
h-index
1 publications · 17 citations
1
h-index
1 publications · 37 citations
1
h-index
1 publications · 94 citations
1
h-index
1–5