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.

458

Publications

16.9K

Citations

980

Authors

388

Institutions

Publications per year

2017–2026

108

Authors

980

  1. JH
    James H. Starnes

    Langley Research Center, United States

    10 publications · 634 citations

    10

    h-index

  2. PD
    P.K. Datta

    Indian Institute of Technology Kharagpur, India

    7 publications · 215 citations

    7

    h-index

  3. LL
    Liviu Librescu

    Virginia Tech, United States

    7 publications · 301 citations

    7

    h-index

  4. AM
    Adrian Murphy

    Queen's University Belfast, United Kingdom

    7 publications · 228 citations

    7

    h-index

  5. RB
    Ruixiang Bai

    Dalian University of Technology, China

    6 publications · 186 citations

    6

    h-index

1–5 of 980

Venues

  1. Composite Structures

    75 publications · 3.4K citations

    35

    h-index

  2. Thin-Walled Structures

    47 publications · 1.7K citations

    25

    h-index

  3. AIAA Journal

    18 publications · 749 citations

    16

    h-index

  4. International Journal of Solids and Structures

    20 publications · 981 citations

    16

    h-index

  5. Computers & Structures

    19 publications · 916 citations

    15

    h-index

1–5