Fuselage Buckling

Fuselage Buckling is a structural instability phenomenon characterized by the sudden lateral deformation of fuselage components under compressive loading, distinguishing it from material failure by its dependence on geometric and stiffness properties rather than strength limits.

15

Publications

627

Citations

41

Authors

20

Institutions

Publications per year

2017–2026

5

Authors

41

  1. AA
    Ahmad Alhajahmad

    Technische Universität Darmstadt, Germany

    2 publications · 92 citations

    2

    h-index

  2. CL
    Christy Lynch

    Queen's University Belfast, United Kingdom

    2 publications · 106 citations

    2

    h-index

  3. AG
    Adam Gibson

    University College London, United Kingdom

    2 publications · 106 citations

    2

    h-index

  4. RS
    Rodney S. Thomson

    UNSW Sydney, Australia

    2 publications · 92 citations

    2

    h-index

  5. CM
    Christian Mittelstedt

    Technische Universität Darmstadt, Germany

    2 publications · 92 citations

    2

    h-index

1–5 of 41

Venues

  1. Composite Structures

    4 publications · 175 citations

    4

    h-index

  2. Thin-Walled Structures

    3 publications · 156 citations

    3

    h-index

  3. International Journal of Mechanical Sciences

    2 publications · 76 citations

    2

    h-index

  4. 1

    h-index

  5. AIAA Journal

    1 publications · 12 citations

    1

    h-index

1–5