Fuselage Vibration Analysis

Fuselage Vibration Analysis is a computational and experimental methodology within aerospace structural dynamics that specifically characterizes the dynamic response and modal behavior of fuselage structures under vibrational loads to assess integrity, performance, and safety.

24

Publications

558

Citations

63

Authors

30

Institutions

Publications per year

2017–2026

2

Authors

63

  1. IC
    Inderjit Chopra

    University of Maryland, College Park, United States

    3 publications · 48 citations

    3

    h-index

  2. JF
    J. F. Wilby

    Berman Center for Outcomes and Clinical Research, United States

    3 publications · 105 citations

    3

    h-index

  3. HY
    Hyeonsoo Yeo

    Ames Research Center, United States

    2 publications · 34 citations

    2

    h-index

  4. FG
    F.L. Gloyna

    Boeing (Australia), Australia

    2 publications · 90 citations

    2

    h-index

  5. GR
    G. R. Eide

    United Aircraft (Russia), Russia

    1 publications · 31 citations

    1

    h-index

1–5 of 63

Venues

  1. AIAA Journal

    3 publications · 82 citations

    3

    h-index

  2. Journal of Sound and Vibration

    JSV · 3 publications · 111 citations

    3

    h-index

  3. Journal of Aircraft

    2 publications · 33 citations

    2

    h-index

  4. Journal of vibration and acoustics

    1 publications · 31 citations

    1

    h-index

  5. Computers & Structures

    1 publications · 21 citations

    1

    h-index

1–5