首页> 外文期刊>Journal of The institution of engineers (India), Series C >The Effect of Fin Pitch on Fluid Elastic Instability of Tube Arrays Subjected to Cross Flow of Water
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The Effect of Fin Pitch on Fluid Elastic Instability of Tube Arrays Subjected to Cross Flow of Water

机译:翅片间距对管阵列的流体弹性不稳定性的影响,对水流流动的管阵

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Abstract Failure of tubes in shell and tube exchangers is attributed to flow induced vibrations of such tubes. There are different excitations mechanisms due to which flow induced vibration occurs and among such mechanisms, fluid elastic instability is the most prominent one as it causes the most violent vibrations and may lead to rapid tube failures within short time. Fluid elastic instability is the fluid–structure interaction phenomenon which occurs when energy input by the fluid force exceeds energy expended in damping. This point is referred as instability threshold and corresponding velocity is referred as critical velocity. Once flow velocity exceeds critical flow velocity, the vibration amplitude increases very rapidly with flow velocity. An experimental program is carried out to determine the critical velocity at instability for plain and finned tube arrays subjected to cross flow of water. The tube array geometry is parallel triangular with cantilever end condition and pitch ratios considered are 2.6 and 2.1. The objective of research is to determine the effect of increase in pitch ratio on instability threshold for plain tube arrays and to assess the effect of addition of fins as well as increase in fin density on instability threshold for finned tube arrays. Plain tube array with two different pitch ratios; 2.1 and 2.6 and finned tube arrays with same pitch ratio; 2.6 but with two different fin pitches; such as fine (10?fpi) and coarse (4?fpi) are considered for the experimentation. Connors’ equation that relates critical velocity at instability to different parameters, on which instability depends, has been used as the basis for analysis and the concept of effective diameter is used for the present investigation. The modal parameters are first suitably modified using natural frequency reduction setup that is already designed and developed to reduce natural frequency and hence to achieve experimental simulation of fluid elastic instability within the limited flow capacity of the pump. The tests are carried out first on plain tube arrays to establish the same as the datum case and results are compared to known results of plain tube arrays and hence the quality of the test rig is also assessed. The fluid elastic vibration tests are then carried out on finned tube arrays with coarse and fine fin pitches and effects of fins and fin pitch on instability threshold are shown. The vibration response of the tube is recorded for each gradually increasing flow rates of water till instability point is reached. The parameters at the instability are then presented in terms of dimensionless parameters to compare them with published results. It is concluded that, arrays with higher pitch ratios are unstable at comparatively higher flow velocities and instability threshold for finned tube arrays is delayed due to addition of the fins. Further, it is concluded that, instability threshold for finned tube arrays with fine fin pitch is delayed compared to coarse fin pitch and hence for increased fin density, instability threshold is delayed. The experimental results in terms of critical velocities obtained for different tube arrays subjected to water cross flow will serve as the base flow rates for air–water cross flow experiments to be conducted in the next phase.
机译:壳体和管交换器中的管子的摘要归因于这种管的流动感应振动。由于发生了流动诱导的振动以及这种机制,流体弹性不稳定性是不同的激励机制,这是最突出的,因为它导致最剧烈的振动,并且可能在短时间内导致快速管失效。流体弹性不稳定性是流体结构相互作用现象,当通过流体力输入超过在阻尼时的能量超过能量时发生的流体结构相互作用现象。该点被称为不稳定性阈值,并且对应的速度被称为关键速度。一旦流动速度超过临界流速,振动幅度随着流速而迅速增加。进行实验程序以确定普通和翅片管阵列的不稳定性处的临界速度,经受交叉水流动。管阵几何形状是平行三角形,悬臂端部条件,俯仰比考虑为2.6和2.1。研究的目的是确定螺节比上增加对普通管阵列的不稳定性阈值的影响,并评估翅片添加的翅片以及翅片管阵列的不稳定性阈值的效果。普通管阵列,具有两种不同的音高比; 2.1和2.6和具有相同间距比的翅片管阵列; 2.6但有两种不同的鳍片;例如考虑细分(10〜FPI)和粗略(4?FPI)进行实验。在不稳定性的不稳定性下将临界速度相关的连接的等式已被用作分析的基础,并且有效直径的概念用于本研究。首先使用已经设计和开发的自然频率减少设置适当地修改模态参数以降低自然频率,从而在泵的有限流动容量内实现流体弹性不稳定的实验模拟。首先在普通管阵列上进行测试,以建立与基准情况相同,并将结果与​​普通管阵列的已知结果进行比较,因此还评估了试验台的质量。然后,示出了流体弹性振动试验,在具有粗糙和细翅片间距的翅片管阵列上进行,并且示出了翅片的翅片和翅片间距对不稳定性阈值的影响。将管的振动响应记录为每个逐渐增加的水的流速,直至达到不稳定点。然后以无稳定性参数呈现不稳定性的参数,以将它们与已发布结果进行比较。得出结论:具有较高俯仰比的阵列在相对较高的流速下不稳定,并且由于添加翅片而延迟了翅片管阵列的不稳定性阈值。此外,结论是,与粗翅片间距相比,延迟了具有细鳍间距的翅片管阵列的不稳定性阈值,因此对于增加的鳍密度,延迟不稳定阈值。对经过水交叉流动的不同管阵列获得的临界速度的实验结果将作为在下相中进行的空气交叉流动实验的基础流速。

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