Full-field operational modal analysis of an aircraft composite panel from the dynamic response in multi-impact test
ISSN: 1424-8220
Année de publication: 2021
Volumen: 21
Número: 5
Pages: 1-14
Type: Article
ISSN: 1424-8220
Année de publication: 2021
Volumen: 21
Número: 5
Pages: 1-14
Type: Article