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STUDY ON EXPLANATION OF DIGITAL IMAGE-PRESSURE MEASUREMENT TECHNOLOGY AND SELF-EXITED OSCILLATION OF FLOW WITH SHOCK WAVES BY THE WAY

STUDY ON EXPLANATION OF DIGITAL IMAGE-PRESSURE MEASUREMENT TECHNOLOGY AND SELF-EXITED OSCILLATION OF FLOW WITH SHOCK WAVES BY THE WAY
数字图像压力测量技术及激波自激流动的解释研究
批准号:
14550165
负责人:
KOJIMA Tadatomo
金额:
$1.54万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2002
资助国家:
日本
项目状态:
已结题
起止时间:
2002 至 2003

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中文摘要
翻译
本文通过流动显示、压力测量和噪声测量等方法,研究了扩张喷管射流的振动、自激振荡和噪声之间的关系。采用纹影法进行瞬态流动显示。总压的压力波动是由一个压力传感器组装到一个总压探头,并进一步测量线性标尺的声压级的噪声测量。利用FFT分析仪对压力和噪声的频率进行了分析。结果表明,总压脉动对喷流噪声有一定的影响。并对汽车消声器模型二维管道内的激波结构进行了研究。通过数值模拟得到的密度分布图与纹影法得到的可视化照片进行了比较。研究了各消声器内的压力、密度、速度分布,并对激波结构进行了分析。结果表明,各模型在激波结构作用和衰减方面存在差异。
英文摘要
In this study, the relation between vibration the self-induced oscillation and noise of jet flow issuing from divergent nozzle were studied by the flow visualization, pressure measurement and noise measurement. The instantaneous flow visualization were taken by schlieren method. The pressure fluctuation of total pressure was measured by a pressure transducer assembled into a total pressure probe and further, the noise of sound pressure level for the linear scale was measured. The frequency of the pressure and noise was analyzed by FFT analyzer. As a result, it was found that the jet noise was influenced by the total pressure fluctuation. Furthermore, the structure of the shock wave occurred in the two dimensions pipe of a muffler model for automobile was studied. The density distribution chart that was obtained by numerical simulation was compared to the visualization photograph by the schlieren method. The distribution of the pressure, density, speed of flow in each muffler was investigated, and shock wave structure was illuminated. As the result, the differences of the shock wave structure action and decrease of each model were clarified.
期刊论文(18)
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会议论文
Tadatomo KOJIMA: "Relation between vibration the self-induced oscillation and noise of jet flow issuing from divergent nozzle"METALLURGICAL AB STRACTS ON LIGHT METALS AND ALLOYS. Vol.XXXV. 204-206 (2002)
Tadatomo KOJIMA:“振动、自激振荡与从发散喷嘴发出的射流噪声之间的关系”轻金属和合金冶金 AB 理论。
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児島忠倫: "広がりノズルからの自励振動とジェット騒音との関連性"可視化情報学会誌. Vol.22, No.1. 475-478 (2002)
小岛忠森:“扩散喷嘴的自激振动与射流噪声之间的关系”可视化信息学会杂志,第 22 卷,第 475-478 期(2002 年)。
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児島忠倫他1名: "非対称性超音速噴流の自励振動と擬似衝撃波構造の解明"近畿大学工業技術研究報告書. 2. 22-26 (2002)
Tadamichi Kojima 等 1:“非对称超音速喷气机的自激振动和伪冲击波结构的阐明”近畿大学工业技术研究报告。
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Tadatomo KOJIMA: "Study on Self-Exited Oscillation and Structure of Pseudo-Shock Waves of Asymmetric Supersonic Jet"近畿大学工学部研究報告. No.36. 139-143 (2002)
小岛忠友:“非对称超音速射流的自激振荡和伪激波结构的研究”近代大学工学部研究报告第36号(2002年)。
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14
    STUDY ON STRUCTURE OF SHOCK WAVES BY DIGITAL IMAGE PROCESSING AND BASIC RESEARCH ON MEASUREMENT TECHNOLOGY OF DIGITAL IMAGE
    • 批准号:
      11650194
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $1.66万
    • 财政年份:
      1999
    • 负责人:
      KOJIMA Tadatomo
    • 依托单位:
    海外基金