Fuselage Strength Analysis
Fuselage Strength Analysis is a computational and theoretical framework within aerospace structural engineering that assesses the load-bearing capacity and integrity of fuselage structures under operational and extreme conditions, distinguished by its focus on material behavior, stress distribution, buckling resistance, and failure criteria specific to aircraft cylindrical and semi-monocoque configurations.
10
Publications
187
Citations
35
Authors
12
Institutions
Publications per year
2017–2026
2
Parents
10
1–5 of 10
35
1
h-index
1
h-index
Sikorsky Aircraft Corporation (United States), United States
1 publications · 10 citations
1
h-index
1
h-index
1
h-index
1–5 of 35
12

Langley Research Center
Hampton, United States
2 h-index
5 publications
78 citations

Boeing (United States)
Chicago, United States
2 h-index
5 publications
100 citations

California State University, Long Beach
Long Beach, United States
1 h-index
3 publications
60 citations

National Academy of Sciences
Washington D.C., United States
1 h-index
1 publications
14 citations

University of Belgrade
Belgrade, Serbia
1 h-index
1 publications
13 citations

Rzeszów University of Technology
Rzeszów, Poland
1 h-index
1 publications
22 citations

Cornell University
Ithaca, United States
1 h-index
1 publications
38 citations
Sikorsky Aircraft Corporation (United States)
Huntsville, United States
1 h-index
1 publications
10 citations
1–8 of 12
2 publications · 34 citations
2
h-index
Conference · 1 publications · 20 citations
1
h-index
1 publications · 13 citations
1
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Repository · 1 publications · 38 citations
1
h-index
1 publications · 22 citations
1
h-index
1–5