Fuselage Cross-section Design

Fuselage Cross-Section Design is a methodological framework within aerospace engineering that defines the geometric and structural configuration of a fuselage’s transverse section, distinguished by its focus on optimizing aerodynamic efficiency, structural integrity, and internal volume allocation in relation to aircraft performance requirements.

11

Publications

213

Citations

38

Authors

8

Institutions

Publications per year

2017–2026

3

Authors

38

  1. VC
    Vittorio Cipolla

    University of Pisa, Italy

    2 publications · 36 citations

    2

    h-index

  2. VB
    Vincenzo Binante

    University of Pisa, Italy

    2 publications · 36 citations

    2

    h-index

  3. HS
    Hirokazu Shoji

    Kawasaki Heavy Industries (Japan), Japan

    1 publications · 26 citations

    1

    h-index

  4. KK
    Karen Karen

    University of Waterloo, Canada

    1 publications · 16 citations

    1

    h-index

  5. MP
    Marco Picchi Scardaoni

    University of Pisa, Italy

    1 publications · 15 citations

    1

    h-index

1–5 of 38

Venues

  1. AIAA Journal

    1 publications · 12 citations

    1

    h-index

  2. AHS International Forum 64

    1 publications · 16 citations

    1

    h-index

  3. Procedia Structural Integrity

    1 publications · 19 citations

    1

    h-index

  4. Journal of Spacecraft and Rockets

    1 publications · 21 citations

    1

    h-index

  5. Journal of Sandwich Structures & Materials

    1 publications · 18 citations

    1

    h-index

1–5