Full-scale modal testing of a Hawk T1A aircraft for benchmarking vibration-based methods (2024)

First Author: Haywood-Alexander M
Attributed to:  Autonomous Modelling Solutions for Operational Structural Dynamic Systems funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.jsv.2024.118295

Publication URI: http://dx.doi.org/10.1016/j.jsv.2024.118295

Type: Journal Article/Review

Parent Publication: Journal of Sound and Vibration