Thermal Buckling

Thermal Buckling is a structural instability phenomenon in which an aircraft structural component undergoes sudden geometric deformation due to compressive thermal stresses induced by temperature changes, distinguished from mechanical buckling by its dependence on thermal loading rather than external mechanical forces.

691

Publications

30.1K

Citations

1.2K

Authors

463

Institutions

Publications per year

2017–2026

262

Authors

1.2K

  1. MR
    M. R. Eslami

    Amirkabir University of Technology, Iran

    29 publications · 2.4K citations

    24

    h-index

  2. YK
    Y. Kiani

    Shahrekord University, Iran

    26 publications · 2K citations

    23

    h-index

  3. AT
    Abdelouahed Tounsi

    Université Djilali de Sidi Bel Abbès, Algeria

    19 publications · 1K citations

    17

    h-index

  4. HS
    Hui‐Shen Shen

    Shanghai Jiao Tong University, China

    15 publications · 1.3K citations

    15

    h-index

  5. AM
    Ashraf M. Zenkour

    King Abdulaziz University, Saudi Arabia

    13 publications · 831 citations

    13

    h-index

1–5 of 1.2K

Venues

  1. Composite Structures

    61 publications · 4.4K citations

    36

    h-index

  2. Journal of Thermal Stresses

    73 publications · 2.9K citations

    34

    h-index

  3. Thin-Walled Structures

    27 publications · 1.4K citations

    22

    h-index

  4. AIAA Journal

    21 publications · 1.3K citations

    19

    h-index

  5. Computers & Structures

    17 publications · 908 citations

    16

    h-index

1–5