Fuselage Structural Optimization
Fuselage Structural Optimization is a systematic engineering methodology that identifies the most efficient structural configuration of an aircraft fuselage by minimizing weight and material usage while satisfying constraints on strength, stiffness, stability, and manufacturability within the domain of aerospace structural design.
13
Publications
364
Citations
37
Authors
11
Institutions
Publications per year
2017–2026
4
Parents
13
1–5 of 13
37
King Fahd University of Petroleum and Minerals, Saudi Arabia
2 publications · 41 citations
2
h-index
2
h-index
2
h-index
2
h-index
2
h-index
1–5 of 37
11

Langley Research Center
Hampton, United States
3 h-index
6 publications
234 citations
Khon Kaen University
Khon Kaen, Thailand
2 h-index
10 publications
205 citations

Boeing (United States)
Chicago, United States
2 h-index
4 publications
164 citations

King Fahd University of Petroleum and Minerals
Dhahran, Saudi Arabia
2 h-index
2 publications
41 citations

Delft University of Technology
Delft, The Netherlands
1 h-index
2 publications
42 citations
European Aquaculture Society
Ostend, Belgium
1 h-index
5 publications
130 citations
University of California, Los Angeles
Los Angeles, United States
1 h-index
1 publications
24 citations
Seattle University
Seattle, United States
1 h-index
1 publications
33 citations
1–8 of 11
IJVD · 2 publications · 41 citations
2
h-index
2 publications · 104 citations
2
h-index
1 publications · 10 citations
1
h-index
1 publications · 13 citations
1
h-index
Conference · 1 publications · 12 citations
1
h-index
1–5