Experimental study of vortex-induced vibrations of a cylinder near a rigid plane boundary in steady flow

Bing Yang, Fuping Gao, Dong-Sheng Jeng, Yingxiang Wu

    Research output: Contribution to journalArticle

    28 Citations (Scopus)

    Abstract

    Abstract In this study, the vortex-induced vibrations of a cylinder near a rigid plane boundary in a steady flow are studied experimentally. The phenomenon of vortex-induced vibrations of the cylinder near the rigid plane boundary is reproduced in the flume. The vortex shedding frequency and mode are also measured by the methods of hot film velocimeter and hydrogen bubbles.Aparametric study is carried out to investigate the influences of reduced velocity, gap-to-diameter ratio, stability parameter and mass ratio on the amplitude and frequency responses of the cylinder. Experimental results indicate: (1) the Strouhal number (St) is around 0.2 for the stationary cylinder near a plane boundary in the sub-critical flow regime; (2) with increasing gap-to-diameter ratio (e0/D), the amplitude ratio (A/D) gets larger but frequency ratio ( f/ fn) has a slight variation for the case of larger values of e0/D(e0/D > 0.66 in this study); (3) there is a clear difference of amplitude and frequency responses of the cylinder between the larger gap-to-diameter ratios (e0/D > 0.66) and the smaller ones (e0/D < 0.3); (4) the vibration of the cylinder is easier to occur and the range of vibration in terms of Vr number becomes more extensive with decrease of the stability parameter, but the frequency response is affected slightly by the stability parameter; (5) with decreasing mass ratio, the width of the lock-in ranges in terms of Vr and the frequency ratio ( f/ fn) become larger.
    Original languageEnglish
    Pages (from-to)51-63
    Number of pages13
    JournalActa Mechanica Sinica
    Volume25
    Issue number1
    DOIs
    Publication statusPublished - 2009

    Fingerprint

    Steady flow
    Frequency response
    Vortex flow
    Velocimeters
    Strouhal number
    Vortex shedding
    Hydrogen

    Keywords

    • Vortex-induced vibration
    • Steady flow
    • Vortex shedding
    • Cylinder

    Cite this

    Yang, Bing ; Gao, Fuping ; Jeng, Dong-Sheng ; Wu, Yingxiang. / Experimental study of vortex-induced vibrations of a cylinder near a rigid plane boundary in steady flow. In: Acta Mechanica Sinica. 2009 ; Vol. 25, No. 1. pp. 51-63.
    @article{184b659ab7744515b4b883038e7d1a23,
    title = "Experimental study of vortex-induced vibrations of a cylinder near a rigid plane boundary in steady flow",
    abstract = "Abstract In this study, the vortex-induced vibrations of a cylinder near a rigid plane boundary in a steady flow are studied experimentally. The phenomenon of vortex-induced vibrations of the cylinder near the rigid plane boundary is reproduced in the flume. The vortex shedding frequency and mode are also measured by the methods of hot film velocimeter and hydrogen bubbles.Aparametric study is carried out to investigate the influences of reduced velocity, gap-to-diameter ratio, stability parameter and mass ratio on the amplitude and frequency responses of the cylinder. Experimental results indicate: (1) the Strouhal number (St) is around 0.2 for the stationary cylinder near a plane boundary in the sub-critical flow regime; (2) with increasing gap-to-diameter ratio (e0/D), the amplitude ratio (A/D) gets larger but frequency ratio ( f/ fn) has a slight variation for the case of larger values of e0/D(e0/D > 0.66 in this study); (3) there is a clear difference of amplitude and frequency responses of the cylinder between the larger gap-to-diameter ratios (e0/D > 0.66) and the smaller ones (e0/D < 0.3); (4) the vibration of the cylinder is easier to occur and the range of vibration in terms of Vr number becomes more extensive with decrease of the stability parameter, but the frequency response is affected slightly by the stability parameter; (5) with decreasing mass ratio, the width of the lock-in ranges in terms of Vr and the frequency ratio ( f/ fn) become larger.",
    keywords = "Vortex-induced vibration, Steady flow, Vortex shedding, Cylinder",
    author = "Bing Yang and Fuping Gao and Dong-Sheng Jeng and Yingxiang Wu",
    year = "2009",
    doi = "10.1007/s10409-008-0221-7",
    language = "English",
    volume = "25",
    pages = "51--63",
    journal = "Acta Mechanica Sinica",
    issn = "0567-7718",
    publisher = "Springer Verlag",
    number = "1",

    }

    Experimental study of vortex-induced vibrations of a cylinder near a rigid plane boundary in steady flow. / Yang, Bing; Gao, Fuping; Jeng, Dong-Sheng; Wu, Yingxiang.

    In: Acta Mechanica Sinica, Vol. 25, No. 1, 2009, p. 51-63.

    Research output: Contribution to journalArticle

    TY - JOUR

    T1 - Experimental study of vortex-induced vibrations of a cylinder near a rigid plane boundary in steady flow

    AU - Yang, Bing

    AU - Gao, Fuping

    AU - Jeng, Dong-Sheng

    AU - Wu, Yingxiang

    PY - 2009

    Y1 - 2009

    N2 - Abstract In this study, the vortex-induced vibrations of a cylinder near a rigid plane boundary in a steady flow are studied experimentally. The phenomenon of vortex-induced vibrations of the cylinder near the rigid plane boundary is reproduced in the flume. The vortex shedding frequency and mode are also measured by the methods of hot film velocimeter and hydrogen bubbles.Aparametric study is carried out to investigate the influences of reduced velocity, gap-to-diameter ratio, stability parameter and mass ratio on the amplitude and frequency responses of the cylinder. Experimental results indicate: (1) the Strouhal number (St) is around 0.2 for the stationary cylinder near a plane boundary in the sub-critical flow regime; (2) with increasing gap-to-diameter ratio (e0/D), the amplitude ratio (A/D) gets larger but frequency ratio ( f/ fn) has a slight variation for the case of larger values of e0/D(e0/D > 0.66 in this study); (3) there is a clear difference of amplitude and frequency responses of the cylinder between the larger gap-to-diameter ratios (e0/D > 0.66) and the smaller ones (e0/D < 0.3); (4) the vibration of the cylinder is easier to occur and the range of vibration in terms of Vr number becomes more extensive with decrease of the stability parameter, but the frequency response is affected slightly by the stability parameter; (5) with decreasing mass ratio, the width of the lock-in ranges in terms of Vr and the frequency ratio ( f/ fn) become larger.

    AB - Abstract In this study, the vortex-induced vibrations of a cylinder near a rigid plane boundary in a steady flow are studied experimentally. The phenomenon of vortex-induced vibrations of the cylinder near the rigid plane boundary is reproduced in the flume. The vortex shedding frequency and mode are also measured by the methods of hot film velocimeter and hydrogen bubbles.Aparametric study is carried out to investigate the influences of reduced velocity, gap-to-diameter ratio, stability parameter and mass ratio on the amplitude and frequency responses of the cylinder. Experimental results indicate: (1) the Strouhal number (St) is around 0.2 for the stationary cylinder near a plane boundary in the sub-critical flow regime; (2) with increasing gap-to-diameter ratio (e0/D), the amplitude ratio (A/D) gets larger but frequency ratio ( f/ fn) has a slight variation for the case of larger values of e0/D(e0/D > 0.66 in this study); (3) there is a clear difference of amplitude and frequency responses of the cylinder between the larger gap-to-diameter ratios (e0/D > 0.66) and the smaller ones (e0/D < 0.3); (4) the vibration of the cylinder is easier to occur and the range of vibration in terms of Vr number becomes more extensive with decrease of the stability parameter, but the frequency response is affected slightly by the stability parameter; (5) with decreasing mass ratio, the width of the lock-in ranges in terms of Vr and the frequency ratio ( f/ fn) become larger.

    KW - Vortex-induced vibration

    KW - Steady flow

    KW - Vortex shedding

    KW - Cylinder

    U2 - 10.1007/s10409-008-0221-7

    DO - 10.1007/s10409-008-0221-7

    M3 - Article

    VL - 25

    SP - 51

    EP - 63

    JO - Acta Mechanica Sinica

    JF - Acta Mechanica Sinica

    SN - 0567-7718

    IS - 1

    ER -