Fuselage Shape Optimization is an academic methodology that systematically refines the geometric configuration of an aircraft fuselage to enhance aerodynamic, structural, and operational performance metrics while adhering to disciplinary constraints.
19
Publications
540
Citations
50
Authors
21
Institutions
Publications per year
2017–2026
6
Parents
Publications
19
Shaping of airplane fuselages for minimum drag
S. S. Dodbele, C. P. van Dam, P. M. H. W. Vijgen et al. · Journal of Aircraft · 1987 · 54 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
1–5 of 19
Authors
50
- JH
3
h-index
- JS
3
h-index
- XY
2
h-index
- SS
2
h-index
- CC
1
h-index
1–5 of 50
Institutions
21
Georgia Institute of Technology
Atlanta, United States
3 h-index
8 publications
305 citations
Boeing (United States)
Chicago, United States
3 h-index
3 publications
113 citations
Langley Research Center
Hampton, United States
3 h-index
4 publications
133 citations
Stanford University
Stanford, United States
2 h-index
6 publications
243 citations
ViGYAN (United States)
Hampton, United States
2 h-index
3 publications
122 citations
Virginia Tech
Blacksburg, United States
1 h-index
1 publications
34 citations
American Institute of Aeronautics and Astronautics
Reston, United States
1 h-index
2 publications
20 citations
Tohoku University
Sendai, Japan
1 h-index
2 publications
30 citations
1–8 of 21
Venues
- Journal of Aircraft
6 publications · 191 citations
6
h-index
- Journal of Manufacturing Science and Engineering
2 publications · 48 citations
2
h-index
- 35th AIAA Applied Aerodynamics Conference
Conference · 1 publications · 19 citations
1
h-index
- Journal of Manufacturing Systems
1 publications · 65 citations
1
h-index
- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
1 publications · 15 citations
1
h-index
1–5