Fuselage Stress Analysis
Fuselage Stress Analysis is a computational and theoretical framework within aerospace structural engineering that specifically evaluates the distribution, magnitude, and criticality of mechanical stresses in the fuselage under operational loads, including pressurization cycles, to ensure structural integrity and safety.
20
Publications
439
Citations
50
Authors
18
Institutions
Publications per year
2017–2026
4
20
1–5 of 20
50
Alagappa Chettiar Government College of Engineering and Technology
2 publications · 41 citations
2
h-index
1 publications · 29 citations
1
h-index
1
h-index
1
h-index
1
h-index
1–5 of 50
18
Georgia Institute of Technology
Atlanta, United States
2 h-index
3 publications
90 citations
Civil Aviation University of China
Tianjin, China
2 h-index
8 publications
317 citations

Cornell University
Ithaca, United States
1 h-index
1 publications
38 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
14 citations
National Academies of Sciences, Engineering, and Medicine
Washington, United States
1 h-index
1 publications
14 citations

Oregon State Hospital
Salem, United States
1 h-index
1 publications
10 citations

Boeing (United States)
Chicago, United States
1 h-index
1 publications
36 citations
Virginia Tech
Blacksburg, United States
1 h-index
1 publications
36 citations
1–8 of 18
5 publications · 61 citations
5
h-index
1 publications · 84 citations
1
h-index
1 publications · 18 citations
1
h-index
1 publications · 13 citations
1
h-index
Conference · 1 publications · 29 citations
1
h-index
1–5