Technical Notes
Mar 31, 2020

Novel Criterion for Evaluation of Stationarity in Nonlinear Structural Dynamics

Publication: Journal of Aerospace Engineering
Volume 33, Issue 4

Abstract

The evaluation of stationarity, such as the widely used steady-state response assessment in stepped-sine testing, is a critical issue in structural dynamics. Stepped-sine excitation is a crucial testing method for nonlinear structures. This method can provide high signal-to-noise measurement data but requires a long measurement time. The disadvantage of lengthy measurements stems mainly from the prolonged time for a structure to reach a steady-state response in each frequency step. Although stepped-sine testing has been applied in numerous studies, there is still no uniform criterion to exactly indicate the moment when the response of a testing structure begins to achieve a steady state. In this study, a precise and novel criterion for evaluating stationarity in nonlinear structural dynamics based on the trend of the squared 2-norm of sinusoidal fitting residual vectors is proposed. Three numerical examples show that the steady-state response determined periodically by the criterion is in good agreement with the results of the theoretical analysis, which demonstrates that the presented criterion not only can assist engineers and researchers in accurately checking steady-state response but also can reduce the unnecessary and redundant waiting time during stepped-sine testing; therefore, the comprehensive performance of stepped-sine testing applied in nonlinear structures can be improved.

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Data Availability Statement

The data used in the three numerical examples are available from the corresponding author by request. Namely, the data used in the first example are used to draw Figs. 58; the data used in the second example are used to draw Figs. 911; and the data used in the third example are used to draw Figs. 13 and 14, respectively.

Acknowledgments

This work was supported by the National Program on Key Basic Research Project (973 Project) [Grant No. 2015CB057704], the National Natural Science Foundation of China [Grant No. 51578107, 51778103], the Science Fund for Creative Research Groups of the National Natural Science Foundation of China [Grant No. 51121005], the Fundamental Research Funds for the Central Universities [Grant No. DUT18LAB07], and the STU Scientific Research Foundation for Talents [Grant No. NTF18012].

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 33Issue 4July 2020

History

Received: Jan 15, 2019
Accepted: Jan 2, 2020
Published online: Mar 31, 2020
Published in print: Jul 1, 2020
Discussion open until: Aug 31, 2020

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Authors

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Ph.D. Student, School of Civil Engineering, State Key Laboratory of Coastal and Offshore Engineering, Dalian Univ. of Technology, No. 2 Linggong Rd., Dalian, Liaoning Province 116024, China. ORCID: https://orcid.org/0000-0001-9544-340X. Email: [email protected]
Dong-Sheng Li [email protected]
Professor, College of Engineering, Guangdong Engineering Center for Structure Safety and Health Monitoring, Shantou Univ., No. 243 Daxue Rd., Shantou, Guangdong Province 515063, China (corresponding author). Email: [email protected]
Hong-Nan Li [email protected]
Professor, School of Civil Engineering, State Key Laboratory of Coastal and Offshore Engineering, Dalian Univ. of Technology, No. 2 Linggong Rd., Dalian, Liaoning Province 116024, China. Email: [email protected]

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