Landing Load Dynamics

Landing Load Dynamics is a scientific framework that characterizes the temporal and spatial distribution of mechanical forces experienced during the impact phase of aerial descent, distinguishing itself by its focus on the interaction between surface properties, vehicle structural compliance, and inertial effects in determining load transmission during touchdown.

70

Publications

2.8K

Citations

225

Authors

106

Institutions

Publications per year

2017–2026

10

Authors

225

  1. HN
    Hong Nie

    Nanjing University of Aeronautics and Astronautics, China

    4 publications · 101 citations

    4

    h-index

  2. BM
    Benjamin Milwitzky

    2 publications · 27 citations

    2

    h-index

  3. AM
    Ajit M.W. Chaudhari

    The Ohio State University, United States

    2 publications · 395 citations

    2

    h-index

  4. CS
    Choongsoo S. Shin

    Sogang University, South Korea

    2 publications · 395 citations

    2

    h-index

  5. TP
    Thomas P. Andriacchi

    Stanford University, United States

    2 publications · 395 citations

    2

    h-index

1–5 of 225

Venues

  1. Journal of Biomechanics

    7 publications · 578 citations

    7

    h-index

  2. Aerospace Science and Technology

    AST · 4 publications · 129 citations

    4

    h-index

  3. Acta Astronautica

    3 publications · 97 citations

    3

    h-index

  4. Journal of Aircraft

    3 publications · 69 citations

    3

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 40 citations

    3

    h-index

1–5