Fuselage Damage Tolerance

Fuselage Damage Tolerance is a structural engineering concept that denotes the inherent capability of a fuselage to sustain specified levels of damage, such as cracks or impact-induced defects, without catastrophic failure and within acceptable safety limits throughout its operational life.

19

Publications

547

Citations

75

Authors

21

Institutions

Publications per year

2017–2026

2

Authors

75

  1. DA
    Damodar Ambur

    Langley Research Center, United States

    3 publications · 49 citations

    3

    h-index

  2. EK
    Erik Kappel

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    1 publications · 19 citations

    1

    h-index

  3. JJ
    J J Wang

    California State University, Long Beach, United States

    1 publications · 47 citations

    1

    h-index

  4. AB
    Andrew Bergan

    Langley Research Center, United States

    1 publications · 31 citations

    1

    h-index

  5. XZ
    Xiang Zhang

    Coventry University, United Kingdom

    1 publications · 32 citations

    1

    h-index

1–5 of 75

Venues

  1. NASA Technical Reports Server (NASA)

    Repository · 4 publications · 88 citations

    4

    h-index

  2. Composite Structures

    2 publications · 47 citations

    2

    h-index

  3. 1

    h-index

  4. Defense Technical Information Center (DTIC)

    Repository · 1 publications · 28 citations

    1

    h-index

  5. Materials science forum

    MSF · Book series · 1 publications · 33 citations

    1

    h-index

1–5