Development of Aeroacoustic Cavity Noise Controlling Devices Utilizing Strong Fluctuation into Turbulent Flows
Development of Aeroacoustic Cavity Noise Controlling Devices Utilizing Strong Fluctuation into Turbulent Flows
批准号:
16360087
负责人:
FUKUNISHI Yu
金额:
$10.07万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
2004
资助国家:
日本
项目状态:
已结题
起止时间:
2004 至 2007
中文摘要
本研究旨在发展一种能有效控制腔体噪声的主动控制装置。我们的策略是在空腔的前缘提供流动分离的相位控制,在那里流动的感受性变得最高。所安装的控制装置可以将具有180度相位差的并排速度波动的波浪图案引入到流动中。压力波动以及由此产生的声波也是180度异相的。在我们的研究中,我们尝试用合成射流来抑制空腔噪声。首先,合成射流产生的扬声器和谐振器的集合。由于发现扬声器的贡献不是对流体颗粒的运动而是对压力波动的贡献,因此确定了产生合成射流的有效位置。因此,通过调节扬声器的声音频率,成功地降低了空腔噪声。此外,另一种控制装置,利用射流振荡器的开发。对于层流分离流,空腔噪声的峰值被成功地抑制到背景噪声水平,谐波分量也从频谱中消失。此外,我们成功地实现了有效的抑制空腔噪声,即使当分离流是湍流时,使用两个同步的射流振荡器沿展向沿着安装。
英文摘要
The purpose of this study has been to develop an energy efficient active control device that can control the cavity noise. Our strategy was to provide the phase control of the flow separation at the leading edge of the cavity, where the receptivity of the flow becomes the highest. The control devices installed can introduce wavy patterns of the velocity fluctuations side-by-side with 180 degrees phase difference into the flow. The pressure fluctuations and hence the sound waves coming out are also 180 degrees out of phase. As a result, the opposite-signed sound waves eventually cancel each other faraway from the source.In our study, the suppression of the cavity noise has been tried by synthetic jets according to the strategy. First, the synthetic jets were generated by the sets of the loudspeakers and the resonators. Because it was found that a loudspeaker's contribution was not to the motion of the fluid particles but to the pressure fluctuation, the effective location to produce the synthetic jets was determined. Consequently, the cavity noise was successfully reduced by adjusting the sound frequency of the loudspeakers.Furthermore, another control device utilizing a fluidic oscillator was developed. For the laminar separating flow, the peak of the cavity noise was successfully suppressed to the background noise level and the harmonic components also disappeared from the spectrum. Moreover, we were successful in achieving an effective suppression of the cavity noise even when the separating flow was turbulent using two synchronized fluidic oscillators installed side by side along the spanwise direction.
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采用 L 网格系统的有限差分法进行涡旋声的 3-D DNS
DOI:
--
发表时间:
2007
期刊:
影响因子:
--
作者:
[米田 広, 渡辺 貴洋, 伊澤 精一郎, 熊 鰲魁, 福西 祐, Yasuhiko SAKAI et al., Y. Nakashima]
通讯作者:
Y. Nakashima
DOI:
10.1063/1.2191847
发表时间:
2006-04
期刊:
Physics of Fluids
影响因子:
4.6
作者:
[O. Inoue;W. Iwakami;N. Hatakeyama]
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O. Inoue;W. Iwakami;N. Hatakeyama
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DOI:
--
发表时间:
2005
期刊:
日本機械学会論文集B編 71巻705号
影响因子:
--
作者:
[K.Ishii, K.Matsuoka, S.Yamamoto, K.Hattori, O.Inoue, O.Inoue, O.Inoue, 福西祐]
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福西祐
キャビティ騒音および遷移境界層制御の試み
空腔噪声和过渡边界层控制的尝试
DOI:
--
发表时间:
2006
期刊:
ながれ, 日本流体力学会誌 25
影响因子:
--
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DOI:
--
发表时间:
2006
期刊:
日本機械学会2006年度年次大会講演論文集 7
影响因子:
--
作者:
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通讯作者:
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共 14 条
Experimental Development of an Aeroacoustic Cavity Noise Controlling Device Utilizing Receptivity of the Flow
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批准号:11355009
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$22.66万
-
财政年份:1999
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负责人:FUKUNISHI Yu
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依托单位:
Active Control of flows using Thin Actuators
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批准号:10450069
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项目类别:Grant-in-Aid for Scientific Research (B).
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资助金额:$8.26万
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财政年份:1998
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负责人:FUKUNISHI Yu
-
依托单位:
Development of a Fuzzy Inferencing Computer Board Which Detects Ordered Motion Patterns From Flow-Visualized Pictures.
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批准号:01850019
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项目类别:Grant-in-Aid for Developmental Scientific Research (B).
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资助金额:$3.33万
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财政年份:1989
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负责人:FUKUNISHI Yu
-
依托单位:
海外基金