Computer Aided Engineering, Volume. 34, Issue 2, 24(2025)

Analysis of random vibration characteristics of spacecraft fastener based on time domain analysis method

LI Liang, CHENG Libo, LI Jiarong, LIU Xia, LI Ping, and YAN Su
Author Affiliations
  • Shaanxi Aerospace Supercomputing Center Co, Ltd, Xi'an 712000, China
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    References(5)

    [5] [5] LU X, ZENG Y, CHEN Y, et al. Transient response characteristics of a bolted flange connection structure with shear pin/cone[J]. Journal of Sound and Vibration, 2017, 395: 240-257. DOI: 10.1016/j.jsv.2017.02.029.

    [6] [6] LIU X T, LIU J H, OUYANG H J, et al. Experimental and numerical studies of bolted joints subjected to torsional excitation[J]. Modern Physics Letters, B: Condensed Matter Physics, Statistical Physics, Applied Physics, 2018, 32(34-36): 18400833. DOI: 10.1142/S0217984918400833.

    [7] [7] ABAD J, MEDEL F J, FRANCO J M. Determination of Valanis model parameters in a bolted lap joint: experimental and numerical analyses of frictional dissipation[J]. International Journal of Mechanical Sciences, 2014, 89: 289-298. DOI: 10.1016/j.ijmecsci.2014.09.014.

    [9] [9] ZHANG M Y, LU L T, WANG W J, et al. The roles of thread wear on self-loosening behavior of bolted joints under transverse cyclic loading[J]. Wear, 2018, 394-395: 30-39. DOI: 10.1016/j.wear.2017.10.006.

    [10] [10] ALLEGRI G, ZHANG X. On the inverse power laws for accelerated random fatigue testing[J]. International Journal of Fatigue, 2008, 30(6): 967-977. DOI: 10.1016/j.ijfatigue.2007.08.023.

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    LI Liang, CHENG Libo, LI Jiarong, LIU Xia, LI Ping, YAN Su. Analysis of random vibration characteristics of spacecraft fastener based on time domain analysis method[J]. Computer Aided Engineering, 2025, 34(2): 24

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    Paper Information

    Received: Nov. 20, 2024

    Accepted: Aug. 22, 2025

    Published Online: Aug. 22, 2025

    The Author Email:

    DOI:10.13340/j.cae.2025.02.005

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