Optimization and engineering verification of excitation scheme for aircraft ground vibration test

Ground vibration test is an important part of aircraft model development and strength verification. In aircraft ground vibration test,an appropriate excitation scheme can significantly shorten the test's period and improve the accuracy of mode identification. In this paper,QR decomposition base...

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Main Authors: CHEN Haoyu, WANG Binwen, SONG Qiaozhi, LI Xiaodong
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2024-10-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023250
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author CHEN Haoyu
WANG Binwen
SONG Qiaozhi
LI Xiaodong
author_facet CHEN Haoyu
WANG Binwen
SONG Qiaozhi
LI Xiaodong
author_sort CHEN Haoyu
collection DOAJ
description Ground vibration test is an important part of aircraft model development and strength verification. In aircraft ground vibration test,an appropriate excitation scheme can significantly shorten the test's period and improve the accuracy of mode identification. In this paper,QR decomposition based on the finite element model is used for global planning of exciter placement,and mode participation is introduced to evaluate the plan's exciting efficiency. The multivariate mode indicator function is used to optimize the exciting force vector for closely spaced modes. Finally,these methods are verified in a small general aircraft's ground vibration test,which significantly improves the test's efficiency and reduces the difficulty of closely spaced modes identification. The excitation scheme optimization method adopted in this article has high engineering application value.
format Article
id doaj-art-8916c489c4cd4829ad5e5b5368fdfd6d
institution OA Journals
issn 1674-8190
language zho
publishDate 2024-10-01
publisher Editorial Department of Advances in Aeronautical Science and Engineering
record_format Article
series Hangkong gongcheng jinzhan
spelling doaj-art-8916c489c4cd4829ad5e5b5368fdfd6d2025-08-20T02:12:38ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902024-10-0115511411910.16615/j.cnki.1674-8190.2024.05.1110.16615/j.cnki.1674-8190.2024.05.11Optimization and engineering verification of excitation scheme for aircraft ground vibration testCHEN Haoyu0WANG Binwen1SONG Qiaozhi2LI Xiaodong3Key Laboratory of Aeronautical Science and Technology for Aeroacoustics and Vibration, Aircraft Strength Research Institute of China, Xi'an 710065, ChinaKey Laboratory of Aeronautical Science and Technology for Aeroacoustics and Vibration, Aircraft Strength Research Institute of China, Xi'an 710065, ChinaKey Laboratory of Aeronautical Science and Technology for Aeroacoustics and Vibration, Aircraft Strength Research Institute of China, Xi'an 710065, ChinaKey Laboratory of Aeronautical Science and Technology for Aeroacoustics and Vibration, Aircraft Strength Research Institute of China, Xi'an 710065, ChinaGround vibration test is an important part of aircraft model development and strength verification. In aircraft ground vibration test,an appropriate excitation scheme can significantly shorten the test's period and improve the accuracy of mode identification. In this paper,QR decomposition based on the finite element model is used for global planning of exciter placement,and mode participation is introduced to evaluate the plan's exciting efficiency. The multivariate mode indicator function is used to optimize the exciting force vector for closely spaced modes. Finally,these methods are verified in a small general aircraft's ground vibration test,which significantly improves the test's efficiency and reduces the difficulty of closely spaced modes identification. The excitation scheme optimization method adopted in this article has high engineering application value.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023250ground vibration testexciting force vectorqr decompositionmode participationmodal identification
spellingShingle CHEN Haoyu
WANG Binwen
SONG Qiaozhi
LI Xiaodong
Optimization and engineering verification of excitation scheme for aircraft ground vibration test
Hangkong gongcheng jinzhan
ground vibration test
exciting force vector
qr decomposition
mode participation
modal identification
title Optimization and engineering verification of excitation scheme for aircraft ground vibration test
title_full Optimization and engineering verification of excitation scheme for aircraft ground vibration test
title_fullStr Optimization and engineering verification of excitation scheme for aircraft ground vibration test
title_full_unstemmed Optimization and engineering verification of excitation scheme for aircraft ground vibration test
title_short Optimization and engineering verification of excitation scheme for aircraft ground vibration test
title_sort optimization and engineering verification of excitation scheme for aircraft ground vibration test
topic ground vibration test
exciting force vector
qr decomposition
mode participation
modal identification
url http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023250
work_keys_str_mv AT chenhaoyu optimizationandengineeringverificationofexcitationschemeforaircraftgroundvibrationtest
AT wangbinwen optimizationandengineeringverificationofexcitationschemeforaircraftgroundvibrationtest
AT songqiaozhi optimizationandengineeringverificationofexcitationschemeforaircraftgroundvibrationtest
AT lixiaodong optimizationandengineeringverificationofexcitationschemeforaircraftgroundvibrationtest