Development of a New Method for Alleviation of Impulsive Aerodynamic - Noise by Means of Water - Sheet
开发一种利用水板减轻脉冲气动噪声的新方法
基本信息
- 批准号:01850044
- 负责人:
- 金额:$ 4.8万
- 依托单位:
- 依托单位国家:日本
- 项目类别:Grant-in-Aid for Developmental Scientific Research
- 财政年份:1989
- 资助国家:日本
- 起止时间:1989 至 1991
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
1. When a compression wave propagates along a tube and reaches its open end, an impulsive wave is emitted outward from its exit toward the surrounding area, which causes an impulsive noise. In the present study, the attenuation and change of waveform of a propagating compression wave, the generation process of the impulsive wave at the exit, and some practical means for alleviation of the impulsive noise have been investigated.2. The strength of a compression wave decreases exponentially with the distance. Numerical calculation has been carried out taking unsteady friction into account instead of steady one. Unsteady friction causes more distortion of the compression waveform and the calculated waveform is in better agreement with the measured one.3. The magnitude of an impulsive wave generated at the open end is nearly proportional to the maximum rate of pressure change of the compression wave coming to the exit. The experimental results of the magnitude at the exit agree well with the results by aeroacoustic analysis where an open end correction is considered.4. A method for alleviation of the magnitude of impulsive noises by means of water-sheet has been developed, and it is confirmed that the present method is quite useful, although the directivity of the controlled noise field is rather strong. Some other methods for reducing the magnitude of impulsive noises such as an application of active noise control system have been developed in the present investigation. The active control system may be the most useful method in these ones.
1.当压缩波沿着管道传播并到达其开口端时,从其出口向周围区域向外发射脉冲波,这引起脉冲噪声。本文研究了压缩波传播过程中波形的衰减和变化,出口处脉冲波的产生过程,以及抑制脉冲噪声的一些实用方法.压缩波的强度随距离呈指数下降。数值计算中考虑了非定常摩擦力而不是定常摩擦力。非定常摩擦使压缩波形畸变较大,计算波形与实测波形吻合较好.在开口端处产生的冲击波的幅度几乎与到达出口的压缩波的最大压力变化率成比例。出口处的实验结果与考虑开口修正的气动声学分析结果吻合较好.本文提出了一种利用水膜抑制脉冲噪声的方法,并证实了这种方法是十分有用的,尽管受控噪声场的方向性很强。在本研究中还提出了其他一些降低脉冲噪声幅度的方法,如应用有源噪声控制系统。主动控制系统是解决这类问题最有效的方法。
项目成果
期刊论文数量(36)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Toshiaki Setoguchi: "A study of negative impulsive wave generator for reducing impulsive noise" Preprint of Japan Society of Mechanical Engineering. (1992)
Toshiaki Setoguchi:“用于减少脉冲噪声的负脉冲波发生器的研究”日本机械工程学会预印本。
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Toshiaki Setoguchi: "Discharge of a weak shock wave from an open end of a tube" Proceedings of the 1989 National Symposium on Shock Wave Phenomena. 31-40 (1990)
Toshiaki Setoguchi:“从管的开口端释放弱冲击波”1989 年全国冲击波现象研讨会论文集。
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- 发表时间:
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- 影响因子:0
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青木 俊之: "圧縮波の開口端からの放出によるパルス音" 日本機械学会講演論文集. 914. 131-133 (1991)
Toshiyuki Aoki:“开放端压缩波发射产生的脉冲声”日本机械工程师学会会议记录 914. 131-133 (1991)。
- DOI:
- 发表时间:
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- 影响因子:0
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- 通讯作者:
Toshiaki Setoguchi: "Reduction of impulsive noise induced by a weak shock wave discharged from an open end of a tube" Preprint of Japan Society of Mechanical Engineers. 914. 134-136 (1991)
Toshiaki Setoguchi:“减少从管的开口端释放的弱冲击波引起的脉冲噪声”日本机械工程师学会预印本。
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- 影响因子:0
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- 通讯作者:
松尾 一泰: "Discharge of a weak shock wave from an open end of a tube" Proceedings of the 1989 National Symposium on Shock Wave Phenomena. 31-40 (1990)
Kazuyasu Matsuo:“从管的开口端释放弱冲击波”1989 年全国冲击波现象研讨会论文集 31-40 (1990)。
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MATSUO Kazuyasu其他文献
MATSUO Kazuyasu的其他文献
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{{ truncateString('MATSUO Kazuyasu', 18)}}的其他基金
Study of Compound Choking Phenomena and Compound Shock Waves in Compressible Internal Flows
可压缩内流复合窒息现象与复合冲击波研究
- 批准号:
17360083 - 财政年份:2005
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Study of Oscillation Characteristics of Shock Trains Formed in Supersonic Internal Flow and its Suppressing Method
超音速内流激波列振荡特性及抑制方法研究
- 批准号:
13450078 - 财政年份:2001
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Study on Aerodynamic Noise induced by Shock Waves in Supersonic Flows and Development of a Method for Reducing the Noise
超音速流中冲击波气动噪声的研究及降噪方法的开发
- 批准号:
09450080 - 财政年份:1997
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$ 4.8万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Development of a New Method for Reducing Impulsive Aerodynamic Noise by means of Active Control Method
主动控制方法降低脉冲气动噪声新方法的开发
- 批准号:
07555380 - 财政年份:1995
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for Scientific Research (A)
Investigation of Choking Phenomena of Supersonic Micro-nozzle Flow with Flashing Evaporation
闪蒸超音速微喷嘴流壅塞现象研究
- 批准号:
06452176 - 财政年份:1994
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$ 4.8万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Development of New Gas Atomizer Supersonic Nozzle System for Super-micro-metal Powder Production
用于超微金属粉末生产的新型气体雾化器超声喷嘴系统的开发
- 批准号:
04555045 - 财政年份:1992
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for Developmental Scientific Research (B)
Post-Shock Expansion Phenomenon in Supersonic Internal Flow
超音速内流中的激波后膨胀现象
- 批准号:
02452119 - 财政年份:1990
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$ 4.8万 - 项目类别:
Grant-in-Aid for General Scientific Research (B)
A study on the suppression of oscillation of pseudo-shock waves by means of passive boundary layer control
无源边界层控制抑制赝激波振荡的研究
- 批准号:
62460094 - 财政年份:1987
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for General Scientific Research (B)
Developemtn of a New Method for Control and %discharge o High Pressure Exhaust Gas by Means of Shock Wave Confinemnt
Developemtn%20of%20a%20New%20Method%20for%20Control%20and%20%discharge%20o%20High%20Pressure%20Exhaust%20Gas%20by%20Means%20of%20Shock%20Wave%20Confinemnt
- 批准号:
61850034 - 财政年份:1986
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for Developmental Scientific Research
A Study of Instability Phenomenon in a Supercritical Diffuser Flow
超临界扩压器流动不稳定现象的研究
- 批准号:
60550127 - 财政年份:1985
- 资助金额:
$ 4.8万 - 项目类别:
Grant-in-Aid for General Scientific Research (C)
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