Full-scale modal testing of a Hawk T1A aircraft for benchmarking vibration-based methods
Marcus Haywood-Alexander, Robin S. Mills, Max D. Champneys, Matthew R., Jones, Matthew S. Bonney, David Wagg, Timothy J. Rogers

TL;DR
This paper presents a comprehensive, openly available benchmark dataset from full-scale modal testing of a Hawk T1A aircraft, aimed at advancing structural dynamics research and validation of identification and prediction methods.
Contribution
It provides a detailed dataset from a full-scale aircraft test, including experimental design, data collection, baseline results, and discussion of challenges for structural dynamics benchmarking.
Findings
Dataset includes frequency and time domain data
Baseline results for identification and prediction tasks
Discussion of dataset-specific challenges
Abstract
Research developments for structural dynamics in the fields of design, system identification and structural health monitoring (SHM) have dramatically expanded the bounds of what can be learned from measured vibration data. However, significant challenges remain in the tasks of identification, prediction and evaluation of full-scale structures. A significant aid in the roadmap to the application of cutting-edge methods to the demands of in-service engineering structures, is the development of comprehensive benchmark datasets. With the aim of developing a useful and worthwhile benchmark dataset for structural dynamics, an extensive testing campaign is presented here. This recent campaign was performed on a decommissioned BAE system Hawk T1A aircraft at the Laboratory for Verification and Validation (LVV) in Sheffield. The aim of this paper is to present the dataset, providing details on…
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