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
Parents
24
1–5 of 24
63
3
h-index
Berman Center for Outcomes and Clinical Research, United States
3 publications · 105 citations
3
h-index
2
h-index
2
h-index
1
h-index
1–5 of 63
30
University of Maryland, College Park
College Park, United States
4 h-index
6 publications
107 citations
Boeing (Australia)
Brisbane, Australia
2 h-index
4 publications
180 citations

Ames Research Center
Mountain View, United States
2 h-index
2 publications
25 citations
National Central University
Taoyuan City, Taiwan
2 h-index
3 publications
73 citations
Mississippi State University
Starkville, United States
1 h-index
2 publications
26 citations

University of Bristol
Bristol, United Kingdom
1 h-index
3 publications
45 citations
Berman Center for Outcomes and Clinical Research
Minneapolis, United States
1 h-index
3 publications
45 citations

University of Auckland
Auckland, New Zealand
1 h-index
1 publications
15 citations
1–8 of 30
3 publications · 82 citations
3
h-index
JSV · 3 publications · 111 citations
3
h-index
2 publications · 33 citations
2
h-index
1 publications · 31 citations
1
h-index
1 publications · 21 citations
1
h-index
1–5