Fuselage Crashworthiness
Fuselage Crashworthiness is a structural performance criterion that denotes the capacity of a fuselage to absorb impact energy and maintain occupant survivability during a crash event through controlled deformation and load management.
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1.2K
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96
Authors
26
Institutions
Publications per year
2017–2026
12
Parents
43
Drop test and crash simulation of a civil airplane fuselage section
Xiaochuan Liu, Jun Guo, Chunyu Bai et al. · Chinese Journal of Aeronautics · 2015 · 59 citations · Full text
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Beihang University
Beijing, China
7 h-index
15 publications
525 citations
Civil Aviation University of China
Tianjin, China
6 h-index
22 publications
696 citations
Italian Aerospace Research Centre
Capua, Italy
5 h-index
8 publications
345 citations

University of Campania "Luigi Vanvitelli"
Caserta, Italy
5 h-index
18 publications
698 citations

DEVCOM Army Research Laboratory
Adelphi, United States
4 h-index
6 publications
149 citations

Hunan University
Changsha, China
4 h-index
7 publications
145 citations

Northwestern Polytechnical University
Xi'an, China
4 h-index
9 publications
250 citations
Wichita State University
Wichita, United States
3 h-index
7 publications
240 citations
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13 publications · 353 citations
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3 publications · 46 citations
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3 publications · 148 citations
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CJA · 2 publications · 93 citations
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2 publications · 70 citations
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