Panel Buckling
Panel Buckling is a structural instability phenomenon in which a flat or curved aircraft structural panel, under in-plane compressive loading, suddenly deforms out-of-plane due to loss of load-carrying capacity, distinguished from global buckling by its localized nature within a larger framed structure.
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16.9K
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980
Authors
388
Institutions
Publications per year
2017–2026
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Langley Research Center
Hampton, United States
23 h-index
59 publications
3.2K citations
Virginia Tech
Blacksburg, United States
14 h-index
28 publications
1.4K citations
Technion – Israel Institute of Technology
Haifa, Israel
13 h-index
21 publications
860 citations
Indian Institute of Technology Kharagpur
Kharagpur, India
12 h-index
22 publications
583 citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
9 h-index
16 publications
588 citations
Dalian University of Technology
Dalian, China
9 h-index
45 publications
2.4K citations

Imperial College London
London, United Kingdom
9 h-index
22 publications
806 citations
Amirkabir University of Technology
Tehran, Iran
8 h-index
16 publications
833 citations
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75 publications · 3.4K citations
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