收稿日期:2024-02-28
修回日期:2024-04-07
接受日期:2024-04-30
出版日期:2024-12-15
发布日期:2024-05-08
通讯作者:
李勇
E-mail:yli@wzu.edu.cn
基金资助:
Yong LI(
), Jianhai YE, Chenghui WANG
Received:2024-02-28
Revised:2024-04-07
Accepted:2024-04-30
Online:2024-12-15
Published:2024-05-08
Contact:
Yong LI
E-mail:yli@wzu.edu.cn
Supported by:摘要:
在开口射流风洞中,采用远场麦克风阵列和粒子图像测速仪(PIV)对等直径三圆柱在不同对称/非对称排列方式下的噪声和流场进行了测试,并通过在圆柱后缘安装实心或多孔分离隔板对噪声进行了控制。实验风速U0=20~50 m/s,基于圆柱直径D的雷诺数ReD =2.7×104~6.8×104。噪声测试发现,对称中心排列的三圆柱总声压随中心位置圆柱2的流向位置x/H在区间(-2,+2)呈现波峰与波谷的变化。同一风速下,波峰处(x/H=-1.75)与波谷处(x/H=-1.5或+0.5)的峰值噪声最大差值可达20 dB,且圆柱2位于上游位置(x/H<0)时的波峰区间噪声水平也明显高于下游位置(x/H>0)。圆柱2沿圆柱1、3中心点等周长圆弧上布置时,三圆柱的噪声与流向布置角度变化不明显。控制研究发现,对于中心流向布置的三圆柱,在上游圆柱后缘安装合适分离隔板可以改变流场并抑制噪声。流向位置x/H=-2时,圆柱2后缘采用长度L/D=1或穿孔率σ=18.4%,L/D=2的分离隔板可降低三圆柱噪声12 dB,如继续偏转隔板到β=30°甚至可达20 dB。流向位置x/H=-2时,在圆柱1、3上安装同类型分离隔板。对于L/D=1的实心隔板,平均降噪5 dB,降噪效果不明显。L/D=2、σ=18.2%的分离隔板,随着偏转角度β增大,降噪效果逐渐增强。当偏转角度β≥20°以上时可降低噪声10 dB以上。PIV测试以及POD分析表明,实验中三圆柱布置方式下的噪声主要来自于上游圆柱涡脱落与下游表面上的涡-固干扰,分离隔板噪声抑制的机理是由于其显著抑制了上游圆柱的涡脱落,即抑制了流场中卡门涡街的形成。
中图分类号:
李勇, 叶剑海, 王成会. 非规则三角排列的三圆柱噪声特性与控制[J]. 航空学报, 2024, 45(23): 630316.
Yong LI, Jianhai YE, Chenghui WANG. Characterization and control of three-cylinder noise in irregular triangular arrangement[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(23): 630316.
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