Fuselage Weight Optimization

Fuselage Weight Optimization is a systematic engineering methodology aimed at minimizing the structural mass of an aircraft fuselage while maintaining required performance, safety, and design constraints through the integrated application of materials selection, configuration design, and analytical modeling techniques.

8

Publications

227

Citations

29

Authors

6

Institutions

Publications per year

2017–2026

1

Authors

29

  1. CK
    Christos Kassapoglou

    Delft University of Technology, Netherlands

    2 publications · 71 citations

    2

    h-index

  2. BK
    Boris Kolesnikov

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

    2 publications · 53 citations

    2

    h-index

  3. MH
    Matthew Hutchison

    Virginia Tech, United States

    1 publications · 27 citations

    1

    h-index

  4. HL
    Heike Lohse-Busch

    University of Leeds, United Kingdom

    1 publications · 41 citations

    1

    h-index

  5. JD
    Jorgen Dahl

    Langley Research Center, United States

    1 publications · 14 citations

    1

    h-index

1–5 of 29

Venues

  1. 2

    h-index

  2. The Aeronautical Journal

    2 publications · 53 citations

    2

    h-index

  3. Thin-Walled Structures

    1 publications · 50 citations

    1

    h-index

  4. elib (German Aerospace Center)

    Repository · 1 publications · 12 citations

    1

    h-index

  5. 31st Aerospace Sciences Meeting

    1 publications · 27 citations

    1

    h-index

1–5