Takeoff Loads

Takeoff Loads is a structural load model that characterizes the dynamic forces and moments imposed on an aircraft during the takeoff phase, distinguishing it from other flight-phase load models by its specific incorporation of engine thrust, aerodynamic lift buildup, ground reaction forces, and runway-induced vibrations under accelerating conditions.

18

Publications

421

Citations

74

Authors

19

Institutions

Publications per year

2017–2026

6

Authors

74

  1. FA
    Farrukh Alvi

    Florida State University, United States

    1 publications · 64 citations

    1

    h-index

  2. ZC
    Zhi Cheng Liu

    1 publications · 27 citations

    1

    h-index

  3. CP
    Cansin Pancaroglu

    Dr. Siyami Ersek Göğüs Kalp Ve Damar Cerrahisi Eğitim Ve Araştırma Hastanesi, Türkiye

    1 publications · 34 citations

    1

    h-index

  4. RA
    Riccardo Adamini

    University of Brescia, Italy

    1 publications · 29 citations

    1

    h-index

  5. ZF
    Zhouwei Fan

    Nanjing University of Aeronautics and Astronautics, China

    1 publications · 24 citations

    1

    h-index

1–5 of 74

Venues

  1. Chinese Journal of Aeronautics

    CJA · 2 publications · 41 citations

    2

    h-index

  2. Journal of Aircraft

    2 publications · 23 citations

    2

    h-index

  3. 2018 Aviation Technology, Integration, and Operations Conference

    Conference · 2 publications · 58 citations

    2

    h-index

  4. Journal of Applied Biomechanics

    JAB · 1 publications · 10 citations

    1

    h-index

  5. Journal of Biomechanics

    1 publications · 23 citations

    1

    h-index

1–5