Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study (2022)

First Author: Dessena G
Attributed to:  Non-linear model reduction for flexible structures funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.3390/aerospace9080438

Publication URI: http://dx.doi.org/10.3390/aerospace9080438

Type: Journal Article/Review

Parent Publication: Aerospace

Issue: 8