Fuselage Structural Optimization

Fuselage Structural Optimization is a systematic engineering methodology that identifies the most efficient structural configuration of an aircraft fuselage by minimizing weight and material usage while satisfying constraints on strength, stiffness, stability, and manufacturability within the domain of aerospace structural design.

13

Publications

364

Citations

37

Authors

11

Institutions

Publications per year

2017–2026

4

Authors

37

  1. SM
    Sadiq M. Sait

    King Fahd University of Petroleum and Minerals, Saudi Arabia

    2 publications · 41 citations

    2

    h-index

  2. JS
    Jaroslaw Sobieszczanski‐Sobieski

    Langley Research Center, United States

    2 publications · 65 citations

    2

    h-index

  3. GQ
    Gary Quinn

    Langley Research Center, United States

    2 publications · 65 citations

    2

    h-index

  4. IK
    Iku Kosaka

    University of Iowa, United States

    2 publications · 65 citations

    2

    h-index

  5. NP
    Nantiwat Pholdee

    Khon Kaen University, Thailand

    2 publications · 41 citations

    2

    h-index

1–5 of 37

Venues

  1. International Journal of Vehicle Design

    IJVD · 2 publications · 41 citations

    2

    h-index

  2. Journal of Aircraft

    2 publications · 104 citations

    2

    h-index

  3. Computers & Structures

    1 publications · 10 citations

    1

    h-index

  4. 1

    h-index

  5. 1

    h-index

1–5