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全风向角下双方柱脉动气动性能试验研究
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Experimental Study on Fluctuating Aerodynamic Characteristics of Two Square Cylinders at Various Incidence Angles
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    摘要:

    为阐明双方柱中上游方柱尾流对下游方柱脉动气动性能的影响,在雷诺数Re = 8.0 × 104均匀来流条件下,完成了间距比P/B = 1.25~5(其中P为柱心距,B为方柱边长)、全风向角α = 0° ~ 90°的双方柱测压风洞试验. 分析了不同P/B条件时下游方柱脉动气动力、升力功率谱、Strouhal数和气动力展向相关性随α的变化规律. 发现P/B < 3时下游方柱的脉动气动力整体上小于单方柱,且α ≥ 40°时几乎不随风向角变化. 但在3 ≤ P/B ≤ 5且0° ≤ α ≤ 30°时下游方柱脉动阻力远大于单方柱. 下游方柱的脉动气动力、升力功率谱和气动力展向相关性随α的变化规律在P/B = 3前后差异显著. P/B < 3时,下游方柱旋涡脱落受到显著抑制;P/B > 3时,下游方柱的脉动气动性能近似于单方柱.

    Abstract:

    To reveal the influence of the wake released from the upstream square cylinder on fluctuating aerodynamic characteristics of the downstream one,wind tunnel tests were carried out to measure the pressure on twin square cylinders,under a uniform inflow condition with a Reynolds number Re of 8.0×104,space ratios P/B of 1.25~5 (where P is the central distance,B is the side length) and various incidence angles of 0° ≤ α ≤ 90°. The variations of fluctuating aerodynamic forces,power spectrums of lift,Strouhal numbers and spanwise aerodynamic correlations with α are investigated considering the multiple space ratios. When P/B < 3,fluctuating forces on the downstream cylinder are roughly smaller than those on a single square cylinder,and they change little at α ≥ 40°. However,when 3 ≤ P/B ≤ 5 and 0° ≤ α ≤ 30°,the fluctuating drag on the downstream cylinder is significantly stronger than that on a single one. The fluctuating forces,power spectrums of lift and spanwise aerodynamic correlations on the downstream cylinder change dramatically when P/B reaches 3. When P/B < 3,vortex shedding from the downstream cylinder is significantly suppressed. When P/B > 3,however,the fluctuating aerodynamic properties of the downstream cylinder become similar to those of a single one.

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引用本文

杜晓庆,成文涛,董浩天?覮,马文勇.全风向角下双方柱脉动气动性能试验研究[J].湖南大学学报:自然科学版,2021,48(11):54~60

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  • 在线发布日期: 2021-11-24
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