Concepedia

Fuselage Stringer Design

Fuselage Stringer Design is an engineering methodology that specifies the structural configuration, material selection, and load-bearing integration of longitudinal stiffening elements within the fuselage shell to optimize weight, strength, and aerodynamic performance.

3

Publications

83

Citations

12

Authors

5

Institutions

Publications per year

2017–2026

1

Parents

Publications

3

A Mixed Optimization Method for Automated Design of Fuselage Structures

J. Sobieszczanski, David D. Loendorf · Journal of Aircraft · 1972 · 52 citations

, , +17

Stiffener Shape Design to Minimize Interior Noise

Stephen P. Engelstad, Kenneth A. Cunefare, E. A. Powell et al. · Journal of Aircraft · 2000 · 19 citations

, , +17

Multi-objective optimisation of assembly fixturing layout for large composite fuselage panel reinforced by frames and stringers

Zhanghao Wang, Dongsheng Li, Liheng Shen et al. · The International Journal of Advanced Manufacturing Technology · 2023 · 14 citations

, , +14

Design and manufacture of a reinforced fuselage structure through automatic laying-up and in-situ consolidation with co-consolidation of skin and stringers using thermoplastic composite materials

I. Martín, K. Fernández, J. Cuenca et al. · Heliyon · 2022 · 12 citations · Full text

, , +17

1–4 of 3

Authors

12

  1. RÉ
    R. Élices

    Foundation for the Research Development and Application of Composite Materials, Spain

    1 publications · 12 citations

    1

    h-index

  2. IM
    I. Martín

    Freie Universität Berlin, Germany

    1 publications · 12 citations

    1

    h-index

  3. JC
    J. Cuenca

    Foundation for the Research Development and Application of Composite Materials, Spain

    1 publications · 12 citations

    1

    h-index

  4. DD
    David D. Loendorf

    Langley Research Center, United States

    1 publications · 52 citations

    1

    h-index

  5. JS
    J. Sobieszczanski

    Langley Research Center, United States

    1 publications · 52 citations

    1

    h-index

1–5 of 12

Institutions

5

  1. Aernnova (Spain)

    Madrid, Spain

    1 h-index

    3 publications

    36 citations

  2. Georgia Institute of Technology

    Atlanta, United States

    1 h-index

    2 publications

    38 citations

  3. Lockheed Martin (United States)

    Bethesda, United States

    1 h-index

    2 publications

    38 citations

  4. Langley Research Center

    Hampton, United States

    1 h-index

    2 publications

    104 citations

  5. Foundation for the Research Development and Application of Composite Materials

    Getafe, Spain

    1 h-index

    3 publications

    36 citations

  6. Beihang University

    Beijing, China

    1 publications

    14 citations

  7. Commercial Aircraft Corporation of China (China)

    Shanghai, China

    1 publications

    14 citations

1–7 of 5

Venues

  1. Journal of Aircraft

    2 publications · 71 citations

    2

    h-index

  2. Heliyon

    1 publications · 12 citations

    1

    h-index

1–3