Fuselage Strength Analysis

Fuselage Strength Analysis is a computational and theoretical framework within aerospace structural engineering that assesses the load-bearing capacity and integrity of fuselage structures under operational and extreme conditions, distinguished by its focus on material behavior, stress distribution, buckling resistance, and failure criteria specific to aircraft cylindrical and semi-monocoque configurations.

10

Publications

187

Citations

35

Authors

12

Institutions

Publications per year

2017–2026

2

Authors

35

  1. SS
    Srdja Stetic-Kozic

    Military Technical Institute, Serbia

    1 publications · 13 citations

    1

    h-index

  2. DW
    David W. Sleight

    Langley Research Center, United States

    1 publications · 16 citations

    1

    h-index

  3. EJ
    ERNEST J. A. GREENWOOD

    Sikorsky Aircraft Corporation (United States), United States

    1 publications · 10 citations

    1

    h-index

  4. MK
    Mirko Kozić

    Military Technical Institute, Serbia

    1 publications · 13 citations

    1

    h-index

  5. BR
    Banavara R. Seshadri

    Langley Research Center, United States

    1 publications · 14 citations

    1

    h-index

1–5 of 35

Venues

  1. International Journal of Fatigue

    2 publications · 34 citations

    2

    h-index

  2. 38th Structures, Structural Dynamics, and Materials Conference

    Conference · 1 publications · 20 citations

    1

    h-index

  3. Journal of Aerospace Engineering

    1 publications · 13 citations

    1

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 1 publications · 38 citations

    1

    h-index

  5. Engineering Failure Analysis

    1 publications · 22 citations

    1

    h-index

1–5