中等间距并列双钝体箱梁气动干扰效应试验
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TU311; TH113

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国家自然科学基金资助项目(51308359,51378323);河北省高等学校科学技术研究基金资助项目(QN20131169,QN2015213)


Experimental Study on Aerodynamic Interference Effect of Twin Parallel Box Girders with Bluff Body in Medial Distance
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    摘要:

    通过节段模型风洞试验研究了中等间距并列双钝体箱梁的气动干扰效应,分析了气动干扰对上下游箱梁三分力系数和涡振的影响。三分力系数试验风攻角的变化范围为-10~10°,双箱梁模型的净间距与单箱梁模型宽之比D/B的变化范围为0.4~1.0。涡振试验风攻角的变化范围为-4~4°,D/B为0.8。研究结果显示:气动干扰对三分力系数的影响主要表现为对下游箱梁的影响,且体现为减小效应;在水平与负攻角来流条件下,气动干扰对上游箱梁涡振的影响较小,对下游箱梁涡振有显著的放大效应;在正攻角来流条件下,气动干扰效应对下游箱梁涡振的影响较小,对上游箱梁涡振有显著的抑制效应。

    Abstract:

    Wind tunnel tests of the sectional models of twin parallel box girders with bluff body in medial distance are performed. Aerodynamic interference effect of twin box girders is studied and influence of aerodynamic interference effect on aerodynamic coefficients and vortex-induced vibration are analyzed. For test of aerodynamic coefficients, the wind attacking angle is ranging from -10°to 10° and D/B (ratio of net spacing of twin box girder models and width of single box girder model)is ranging from 0.4 to 1. For test of vortex-induced vibration, the wind attacking angle is ranging from -4°to 4 and D/B is 0.8. The research results show that aerodynamic interference effect on aerodynamic coefficients of forward box girder can be neglected. Aerodynamic interference effect on aerodynamic coefficients of leeward box girder is shown as reducing effect. Under zero and negative wind attacking angles,aerodynamic interference effect on vortex-induced vibration is slight for forward box girder and shown as remarkable amplification effect for leeward box girder. Under positive wind attacking angles,aerodynamic interference effect on vortex-induced vibration is slight for leeward box girder and shown as remarkable reducing effect for forward box girder.

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  • 在线发布日期: 2017-11-09
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