Classical Laminate Theory is a structural analysis framework within composite materials mechanics that models the behavior of laminated plates by assuming linear elasticity, perfect bonding between layers, and negligible transverse shear deformation, thereby enabling the prediction of stress and strain distributions through the laminate thickness based on classical plate theory.
180
Publications
13.3K
Citations
454
Authors
195
Institutions
Publications per year
2017–2026
47
Publications
180
1–5 of 180
Authors
454
- JP
5
h-index
- NJN. J. Pagano
United States Air Force Research Laboratory, United States
5 publications · 2.9K citations
5
h-index
- MW
4
h-index
- MM
4
h-index
- AF
3
h-index
1–5 of 454
Institutions
195
Virginia Tech
Blacksburg, United States
8 h-index
11 publications
2.2K citations
Politecnico di Torino
Turin, Italy
5 h-index
20 publications
1K citations
Georgia Institute of Technology
Atlanta, United States
5 h-index
10 publications
271 citations
University of Ottawa
Ottawa, Canada
4 h-index
9 publications
425 citations
University of Alberta
Edmonton, Canada
4 h-index
6 publications
631 citations
Imperial College London
London, United Kingdom
3 h-index
4 publications
119 citations
United States Air Force Research Laboratory
Wright-Patterson AFB, United States
3 h-index
4 publications
2.2K citations
Chinese Academy of Sciences
Beijing, China
3 h-index
12 publications
1.5K citations
1–8 of 195
Venues
- Journal of Composite Materials
JCM · 28 publications · 5.5K citations
21
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- AIAA Journal
10 publications · 1K citations
10
h-index
- Journal of Reinforced Plastics and Composites
JRPC · 8 publications · 528 citations
8
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- Composites Science and Technology
7 publications · 691 citations
7
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- Composite Structures
7 publications · 599 citations
7
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1–5