Skin-stringer Buckling
Skin-Stringer Buckling is a structural instability phenomenon in aerospace engineering wherein the interconnected skin and stringer components of an aircraft panel buckle collaboratively under compressive loading, distinguished from isolated buckling modes by the coupled behavior and load transfer between the thin skin and its stiffening stringers.
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78
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2017–2026
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Characterisation of impact damage in skin-stringer composite structures
E.S. Greenhalgh, Sarah Bishop, D. Bray et al. · Composite Structures · 1996 · 44 citations
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Delft University of Technology
Delft, The Netherlands
4 h-index
8 publications
168 citations

University of Campania "Luigi Vanvitelli"
Caserta, Italy
3 h-index
11 publications
379 citations
Airbus (Germany)
Hamburg, Germany
2 h-index
2 publications
45 citations
Politecnico di Milano
Milan, Italy
2 h-index
4 publications
64 citations
University of Southampton
Southampton, United Kingdom
2 h-index
3 publications
156 citations

Rzeszów University of Technology
Rzeszów, Poland
1 h-index
3 publications
60 citations

McGill University
Montreal, Canada
1 h-index
3 publications
111 citations
Royal Aeronautical Society
London, United Kingdom
1 h-index
1 publications
32 citations
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JSV · 4 publications · 161 citations
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4 publications · 132 citations
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3 publications · 111 citations
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2 publications · 34 citations
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1 publications · 49 citations
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