Composite Fuselage Design

Composite Fuselage Design is a structural engineering methodology within aerospace design that specifically employs fiber-reinforced polymer composite materials to achieve lightweight, high-strength airframe configurations through integrated material and structural optimization distinct from conventional metallic fuselage construction.

44

Publications

1.5K

Citations

116

Authors

40

Institutions

Publications per year

2017–2026

6

Authors

116

  1. KE
    Karen E. Jackson

    Langley Research Center, United States

    7 publications · 125 citations

    7

    h-index

  2. EL
    Edwin L. Fasanella

    Langley Research Center, United States

    5 publications · 98 citations

    5

    h-index

  3. FJ
    F. J. Balena

    Lockheed Martin (United States), United States

    3 publications · 58 citations

    3

    h-index

  4. XY
    Xiaowei Yue

    Virginia Tech, United States

    3 publications · 123 citations

    3

    h-index

  5. JS
    Jianjun Shi

    Georgia Institute of Technology, United States

    3 publications · 123 citations

    3

    h-index

1–5 of 116

Venues

  1. Journal of Aircraft

    4 publications · 167 citations

    4

    h-index

  2. elib (German Aerospace Center)

    Repository · 3 publications · 57 citations

    3

    h-index

  3. CEAS Aeronautical Journal

    2 publications · 35 citations

    2

    h-index

  4. Journal of the American Helicopter Society

    2 publications · 27 citations

    2

    h-index

  5. 1

    h-index

1–5