A flow past a circular-section cylinder with a perforated conic shroud, in which the perforation is located at the peak of the conic disturbance as the shroud installed on the cylinder and uniformly distributed with s...A flow past a circular-section cylinder with a perforated conic shroud, in which the perforation is located at the peak of the conic disturbance as the shroud installed on the cylinder and uniformly distributed with several circular holes,is numerically simulated at a Reynolds number of 100. Two factors in the perforation are taken into account, i.e. the attack angle relative to the direction of incoming flow and diameter of holes. The effect of such perforation on the drag, lift and vortex-shedding frequency is mainly investigated. Results have shown that variation of the attack angle has a little effect, especially on the drag and vortex-shedding frequency, except in certain cases due to the varied vortex-shedding patterns in the near wake. The increasing hole diameter still exhibits a little effect on the drag and frequency of vortex shedding, but really reduces the lift, in particular at larger wavelength, such as the lift reduction reaching almost 66%–68% after introducing the perforation.展开更多
在分析前人实验结论和平板闸门自激振动机理的基础上,将结构—尾流振子模型应用到闸门垂向自激振动的研究中,振子模型采用von der por方程,在结构的控制方程中合理地加入了附加质量项。通过确定模型其他参数并对模型进行计算得到闸门稳...在分析前人实验结论和平板闸门自激振动机理的基础上,将结构—尾流振子模型应用到闸门垂向自激振动的研究中,振子模型采用von der por方程,在结构的控制方程中合理地加入了附加质量项。通过确定模型其他参数并对模型进行计算得到闸门稳定自激振动(共振区)下的垂向振动峰值和频率比。计算值和实测值能较好地吻合,从而实现了影响闸门自激振动参数的整合及对闸门自激振动的定量研究,为进一步深入分析闸门自激振动的机理提供了更加可靠的依据。展开更多
基金supported by the National Key Scientific Instrument and Equipment Development Program of China(Grant No.2011YQ120048)
文摘A flow past a circular-section cylinder with a perforated conic shroud, in which the perforation is located at the peak of the conic disturbance as the shroud installed on the cylinder and uniformly distributed with several circular holes,is numerically simulated at a Reynolds number of 100. Two factors in the perforation are taken into account, i.e. the attack angle relative to the direction of incoming flow and diameter of holes. The effect of such perforation on the drag, lift and vortex-shedding frequency is mainly investigated. Results have shown that variation of the attack angle has a little effect, especially on the drag and vortex-shedding frequency, except in certain cases due to the varied vortex-shedding patterns in the near wake. The increasing hole diameter still exhibits a little effect on the drag and frequency of vortex shedding, but really reduces the lift, in particular at larger wavelength, such as the lift reduction reaching almost 66%–68% after introducing the perforation.
文摘在分析前人实验结论和平板闸门自激振动机理的基础上,将结构—尾流振子模型应用到闸门垂向自激振动的研究中,振子模型采用von der por方程,在结构的控制方程中合理地加入了附加质量项。通过确定模型其他参数并对模型进行计算得到闸门稳定自激振动(共振区)下的垂向振动峰值和频率比。计算值和实测值能较好地吻合,从而实现了影响闸门自激振动参数的整合及对闸门自激振动的定量研究,为进一步深入分析闸门自激振动的机理提供了更加可靠的依据。
