Fuselage Stress Analysis

Fuselage Stress Analysis is a computational and theoretical framework within aerospace structural engineering that specifically evaluates the distribution, magnitude, and criticality of mechanical stresses in the fuselage under operational loads, including pressurization cycles, to ensure structural integrity and safety.

20

Publications

439

Citations

50

Authors

18

Institutions

Publications per year

2017–2026

4

Authors

50

  1. GR
    G. Raj Kumar

    Alagappa Chettiar Government College of Engineering and Technology

    2 publications · 41 citations

    2

    h-index

  2. RU
    R Udaya Prakash

    1 publications · 29 citations

    1

    h-index

  3. MD
    M. Di Sciuva

    Politecnico di Torino, Italy

    1 publications · 12 citations

    1

    h-index

  4. SM
    Sérgio M. O. Tavares

    Universidade do Porto, Portugal

    1 publications · 15 citations

    1

    h-index

  5. MR
    Marshall Rouse

    Langley Research Center, United States

    1 publications · 10 citations

    1

    h-index

1–5 of 50

Venues

  1. 5

    h-index

  2. Progress in Aerospace Sciences

    1 publications · 84 citations

    1

    h-index

  3. AIAA Journal

    1 publications · 18 citations

    1

    h-index

  4. International Journal of Fatigue

    1 publications · 13 citations

    1

    h-index

  5. IOP Conference Series Materials Science and Engineering

    Conference · 1 publications · 29 citations

    1

    h-index

1–5