Fuselage Composite Structures

Fuselage Composite Structures is a structural engineering construct that refers to the load-bearing airframe configuration of an aircraft's main body, distinguished by its primary construction from fiber-reinforced polymeric or advanced composite materials engineered to optimize strength-to-weight ratios and resist aerodynamic and operational stresses.

104

Publications

3.5K

Citations

326

Authors

90

Institutions

Publications per year

2017–2026

29

Authors

326

  1. LB
    L. B. Ilcewicz

    Boeing (United States), United States

    6 publications · 106 citations

    7

    h-index

  2. KE
    Karen E. Jackson

    Langley Research Center, United States

    6 publications · 117 citations

    6

    h-index

  3. FD
    Francesco Di Caprio

    Italian Aerospace Research Centre, Italy

    5 publications · 185 citations

    5

    h-index

  4. EL
    Edwin L. Fasanella

    Langley Research Center, United States

    5 publications · 99 citations

    5

    h-index

  5. BF
    Brian Flynn

    University of Edinburgh, United Kingdom

    3 publications · 63 citations

    4

    h-index

1–5 of 326

Venues

  1. Composite Structures

    4 publications · 229 citations

    5

    h-index

  2. Journal of Aircraft

    5 publications · 169 citations

    5

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 5 publications · 69 citations

    5

    h-index

  4. elib (German Aerospace Center)

    Repository · 4 publications · 119 citations

    4

    h-index

  5. Composites Science and Technology

    3 publications · 133 citations

    3

    h-index

1–5