Full-field operational modal analysis of an aircraft composite panel from the dynamic response in multi-impact test

  1. Molina-Viedma, Á.
  2. López-Alba, E.
  3. Felipe-Sesé, L.
  4. Díaz, F.

ISSN: 1424-8220

Year of publication: 2021

Volume: 21

Issue: 5

Pages: 1-14

Type: Article

DOI: 10.3390/S21051602 GOOGLE SCHOLAR lock_openOpen access editor