Fuselage Buckling
Fuselage Buckling is a structural instability phenomenon characterized by the sudden lateral deformation of fuselage components under compressive loading, distinguishing it from material failure by its dependence on geometric and stiffness properties rather than strength limits.
15
Publications
627
Citations
41
Authors
20
Institutions
Publications per year
2017–2026
5
15
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41
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20

Technische Universität Darmstadt
Darmstadt, Germany
2 h-index
4 publications
184 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
2 h-index
4 publications
238 citations
Queen's University Belfast
Belfast, United Kingdom
2 h-index
6 publications
318 citations

Istanbul Technical University
Istanbul, Türkiye
1 h-index
3 publications
102 citations

UNSW Sydney
Sydney, Australia
1 h-index
2 publications
38 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
1 h-index
2 publications
40 citations
Italian Aerospace Research Centre
Capua, Italy
1 h-index
2 publications
94 citations

University of Canterbury
Christchurch, New Zealand
1 h-index
3 publications
408 citations
1–8 of 20
4 publications · 175 citations
4
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3 publications · 156 citations
3
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2 publications · 76 citations
2
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Conference · 1 publications · 20 citations
1
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1 publications · 12 citations
1
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1–5