Structural Load Limits

Structural Load Limits is the maximum stress or force a flight vehicle's airframe can withstand without experiencing permanent deformation or failure, defined by engineering specifications and certification standards to ensure structural integrity under expected aerodynamic, inertial, and environmental conditions during flight.

36

Publications

983

Citations

80

Authors

38

Institutions

Publications per year

2017–2026

3

Variants

Structural Load Limitations

Authors

80

  1. YL
    Yuebao Lei

    EDF Energy (United Kingdom), United Kingdom

    4 publications · 67 citations

    4

    h-index

  2. JF
    Joseph F. Horn

    Pennsylvania State University, United States

    2 publications · 64 citations

    2

    h-index

  3. QD
    Qinfeng Di

    Shanghai University, China

    2 publications · 38 citations

    2

    h-index

  4. ZG
    Zengliang Gao

    Zhejiang University of Technology, China

    2 publications · 33 citations

    2

    h-index

  5. NS
    Nilesh Sahani

    Pennsylvania State University, United States

    2 publications · 64 citations

    2

    h-index

1–5 of 80

Venues

  1. Journal of Pressure Vessel Technology

    3 publications · 67 citations

    3

    h-index

  2. 3

    h-index

  3. International Journal of Solids and Structures

    3 publications · 178 citations

    3

    h-index

  4. Journal of Aircraft

    2 publications · 65 citations

    2

    h-index

  5. Engineering Structures

    2 publications · 42 citations

    2

    h-index

1–5