Wing Buckling Analysis

Wing Buckling Analysis is a structural engineering methodology that assesses the critical load conditions under which a wing's components lose stability through sudden deformation, distinguishing itself from general structural analyses by focusing specifically on elastic instability mechanisms in thin-walled aerospace structures.

32

Publications

746

Citations

79

Authors

32

Institutions

Publications per year

2017–2026

5

Authors

79

  1. RK
    Rakesh K. Kapania

    Virginia Tech, United States

    4 publications · 78 citations

    4

    h-index

  2. MB
    M.C. Bowering

    Airbus (United Kingdom), United Kingdom

    2 publications · 62 citations

    2

    h-index

  3. FA
    Fernando Almeida

    INESC TEC, Portugal

    2 publications · 62 citations

    2

    h-index

  4. DK
    David Kennedy

    Cardiff University, United Kingdom

    2 publications · 33 citations

    2

    h-index

  5. LD
    Luciano Demasi

    San Diego State University, United States

    2 publications · 39 citations

    2

    h-index

1–5 of 79

Venues

  1. Journal of Aircraft

    6 publications · 236 citations

    6

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 79 citations

    3

    h-index

  3. 2

    h-index

  4. Journal of the Structural Division

    1 publications · 27 citations

    1

    h-index

  5. CEAS Aeronautical Journal

    1 publications · 13 citations

    1

    h-index

1–5