Fuselage Deformation Analysis

Fuselage Deformation Analysis is a computational and experimental methodology within aerospace structural engineering that specifically characterizes the spatial and temporal changes in fuselage geometry under operational loads, distinguishing itself by its focus on strain distribution, buckling behavior, and elasticity in thin-walled aircraft pressure cabins.

17

Publications

457

Citations

47

Authors

24

Institutions

Publications per year

2017–2026

6

Authors

47

  1. KV
    K. Veeranjaneyulu

    University of Waterloo, Canada

    1 publications · 12 citations

    1

    h-index

  2. PX
    Pu Xue

    Northwestern Polytechnical University, China

    1 publications · 27 citations

    1

    h-index

  3. MB
    Maher Bouazizi

    Tunis El Manar University, Tunisia

    1 publications · 17 citations

    1

    h-index

  4. EJ
    ERNEST J. A. GREENWOOD

    Sikorsky Aircraft Corporation (United States), United States

    1 publications · 10 citations

    1

    h-index

  5. KK
    K. Khushal

    University of Waterloo, Canada

    1 publications · 12 citations

    1

    h-index

1–5 of 47

Venues

  1. 2

    h-index

  2. Journal of Engineering Mechanics

    1 publications · 29 citations

    1

    h-index

  3. Thin-Walled Structures

    1 publications · 17 citations

    1

    h-index

  4. 1

    h-index

  5. Composite Structures

    1 publications · 94 citations

    1

    h-index

1–5