Full-scale modal testing of a Hawk T1A aircraft for benchmarking vibration-based methods-Reference-Cited by-同舟云学术

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

Published:2024-04 Issue: Volume:576 Page:118295
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Haywood-Alexander Marcus^ORCID,Mills Robin S.,Champneys Max D.,Jones Matthew R.,Bonney Matthew S.,Wagg David,Rogers Timothy J.

Funder

Alan Turing Institute

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Reference23 articles.

1. Fundamentals of Structural Dynamics;Craig,2006

2. Introduction to Structural Dynamics and Aeroelasticity;Hodges,2011

3. Review and assessment of model updating for non-linear, transient dynamics;Hemez;Mech. Syst. Signal Process.,2001

4. Past, present and future of nonlinear system identification in structural dynamics;Kerschen;Mech. Syst. Signal Process.,2006

5. Nonlinearity in Structural Dynamics: Detection, Identification and Modelling;Worden,2019

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Global Calibration Method for Multi-View-Based Vibration Measurement of Large Structures;2024

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