Fuselage Crashworthiness

Fuselage Crashworthiness is a structural performance criterion that denotes the capacity of a fuselage to absorb impact energy and maintain occupant survivability during a crash event through controlled deformation and load management.

43

Publications

1.2K

Citations

96

Authors

26

Institutions

Publications per year

2017–2026

12

Authors

96

  1. EL
    Edwin L. Fasanella

    Langley Research Center, United States

    6 publications · 107 citations

    6

    h-index

  2. YR
    Yiru Ren

    Hunan University, China

    6 publications · 177 citations

    6

    h-index

  3. KE
    Karen E. Jackson

    Langley Research Center, United States

    6 publications · 121 citations

    6

    h-index

  4. HM
    Haolei Mou

    Civil Aviation University of China, China

    5 publications · 174 citations

    5

    h-index

  5. FD
    Francesco Di Caprio

    Italian Aerospace Research Centre, Italy

    5 publications · 198 citations

    5

    h-index

1–5 of 96

Venues

  1. International Journal of Crashworthiness

    13 publications · 353 citations

    11

    h-index

  2. 3

    h-index

  3. Progress in Aerospace Sciences

    3 publications · 148 citations

    3

    h-index

  4. Chinese Journal of Aeronautics

    CJA · 2 publications · 93 citations

    2

    h-index

  5. AIAA Journal

    2 publications · 70 citations

    2

    h-index

1–5