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A RESPONSE MODEL FOR VORTEX INDUCED VIBRATIONS IN LOW KC NUMBER FLOWS

机译:低KC数流中涡激振动的响应模型。

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Vortex induced vibrations (VIV) are generally less critical in wave dominated flow conditions than in pure current flows. A steady state response needs time to build up and continuous variation in flow velocity generally reduces the vibration amplitudes. For low Keulegan-Carpenter (KC) flows in-line VIV is generally removed entirely, replaced by forced response at the wave frequency, while cross-flow vibration amplitudes are reduced. For large KC numbers, the wave induced flow behaves similarly to a current and the oscillatory nature of the flow no longer influences the VIV response as much. Empirical models to predict the influence of waves in VIV design of offshore cylindrical structures are formulated in offshore design codes. For most flow regimes the models are sound and supported by a solid base of empirical test data. There are, however, exceptions - particularly for the low KC number regime, defined here as LKCR. For such flows the oscillating pressure differentials which cause vortex induced vibrations are no longer governed by traditional dimensionless parameters such as the reduced velocity, but instead the oscillating lift is governed by the ratio between the eigen-frequency of the structure and the wave frequency. Particularly, the frequency of the lift force is twice the wave frequency in regular waves. In irregular wave conditions there are necessarily also spectral peaks at both the actual wave frequency and at three times the wave frequency, but the governing spectral density is concentrated at two times the wave frequency. The present study introduces a novel response model to conservatively assess cross-flow VIV in LKCR.
机译:在波为主的流动条件下,涡流感应振动(VIV)的重要性通常不如在纯电流条件下重要。稳态响应需要时间来建立,并且流速的连续变化通常会减小振动幅度。对于低Keulegan-Carpenter(KC)流量,通常会完全删除管道VIV,取而代之的是在波频率下的强制响应,同时减小了横流振动幅度。对于较大的KC数,波感应流的行为类似于电流,并且流的振荡性质不再对VIV响应产生太大影响。在海上设计规范中制定了用于预测波浪在海上圆柱结构VIV设计中影响的经验模型。对于大多数流动情况,模型都是可靠的,并有经验测试数据的坚实基础。但是,也有例外-特别是对于低KC编号体制(在此定义为LKCR)。对于这种流动,引起涡流引起的振动的振荡压力差不再受传统的无量纲参数(例如降低的速度)控制,而是由结构的本征频率与波频率之间的比率决定振荡升程。特别地,升力的频率是规则波中的波频率的两倍。在不规则波情况下,在实际波频率和波频率的三倍处也必定会出现频谱峰值,但是控制频谱密度集中在波频率的两倍处。本研究介绍了一种新型的响应模型,以保守地评估LKCR中的错流VIV。

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