• Search Research Projects
  • Search Researchers
  • How to Use
  1. Back to previous page

MECHANISM OF THE TRANSFORMATION OF PRESSURE FLUCTUATION PRODUCED BY KARMAN VORTEX SHEDDING INTO NOISE

Research Project

Project/Area Number 03650149
Research Category

Grant-in-Aid for General Scientific Research (C)

Allocation TypeSingle-year Grants
Research Field Fluid engineering
Research InstitutionKYUSHU UNIVERSITY

Principal Investigator

FUKANO Tohru  KYUSHU UNIVERSITY,MECHANICAL ENGINEERING, PROFESSOR, 工学部, 教授 (60037968)

Co-Investigator(Kenkyū-buntansha) KADOGUCHI Katsuhiko  KYUSHU UNIVERSITY, MECHANICAL ENGINEERING, ASSOCIATE PROFESSOR, 工学部, 助教授 (60194867)
HAYASHI Hidechito  NAGASAKI UNIVERSITY, MECHANICAL ENGINEERING, ASSOCIATE PROFESSOR, 工学部, 助教授 (10173022)
Project Period (FY) 1991 – 1992
Project Status Completed (Fiscal Year 1992)
Budget Amount *help
¥2,100,000 (Direct Cost: ¥2,100,000)
Fiscal Year 1992: ¥600,000 (Direct Cost: ¥600,000)
Fiscal Year 1991: ¥1,500,000 (Direct Cost: ¥1,500,000)
KeywordsNoise / Discrete Frequency Noise / Karman Vortex / Broad Band Noise / Uniform Flow Field / Rotating Flow Field / 圧力変動 / NACA翼
Research Abstract

It is theoretically and experimentally investigated that the generated noise is closely related with the characteristics of the velocity fluctuation in the near wakes of a blade,NACA 0008 or NACA 0015 placed in a uniform oncoming flow,and in the near wake of a rotating flat plate. The results are summarized as follows:(1)In the case of a thicker blade,NACA 0015,the discrete frequency noise is generated if the attack angle theta is less than about 5 degree. The flow on the pressure side, separates in this case just upstream of the trailing edge of the blade and the Karman vortex street generates,which is the cause to generate the discrete frequency noise. (2)In the case of a thinner blade,NACA 0008,the DFN does not occur if theta=0,because there is no location where adverse pressure gradient is intense. However if there is some attack angle,even if it is small,the flow separates near the leading edge of the blade due to its relatively sharp geometry. Then discrete frequency noise generates. (3)In the case of NACA 0008 blade periodic velocity fluctuation is actually generated relatively far from the blade trailing edge,the DFN,however,does not occur. The reason of this is the flow attached up to the blade trailing edge. This fact shows clearly that the necessary condition of the generation of DFN is the existence of a large dead flow region in the near wake. (4)Although the oncoming flow is sheared in the span direction as in the case of the rotating flow field,DFN occurs. This means the mechanism of the generation of DFN is fundamentally the same that in the uniform main flow. (5)The broad band nature of the spectrum of noise generated from the rotating flat plate can be theoretically explained by the physical model in which the tonal noises are generated locally by the periodic velocity fluctuations due to each Karman vortex shedding and they are integrated in the blade span direction.

Report

(3 results)
  • 1992 Annual Research Report   Final Research Report Summary
  • 1991 Annual Research Report
  • Research Products

    (18 results)

All Other

All Publications (18 results)

  • [Publications] 深野 徹,福原 稔 松尾 哲,林 秀千人: "回転する単独平板翼の後流に関する研究(第2報,迎え角が小さい場合の流動様相に与える先端すきまの影響)" 日本機械学会論文集(B編). 57-535. 891-897 (1991)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] 深野 徹,福原 稔 磯部 浩,広中 康生 林 秀千人: "回転する単独平板翼の後流に関する研究(第3報,速度の周期変動現象に及ぼす後縁形状の影響)" 日本機械学会論文集(B編). 58-551. 2087-2092 (1992)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] Fukano,T.,Hayashi,H.,Isobe,H.,Hironaka,Y.& Fukuhara,M.,: "Periodic Velocity Fluctuation in the Near Wake of a Rotating Flat-Plate Blade and its Roll in the Generation of Turbulent Noise" ACOUSTICAL EFFECTS IN FSI(ASME WAM). 4. 1-14 (1992)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] 林 秀千人 深野 徹: "一様流中のNACA対称翼から発生する離散周波数騒音に関する実験的研究(翼厚による発生機構の差異)" 日本機械学会論文集(B編).

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] 深野 徹,濱川 洋充 林 秀千人,猿渡 博孝: "回転する単独平板翼から発生する広帯域騒音のスペクトル密度分布の予測に関する研究" 日本機械学会論文集(B編).

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] T.Fukano: "The Wake of a Rotating Flat Plate Blade(Part2,The effect of tip clearance on the flow pattern in the case of a small attack angle)" Trans.JSME. 57-535. 891-897 (1991)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] T.Fukano: "The Wake of a Rotating Flat Plate Blade(Part3,The effect of trailing edge geometry on the periodic velocity fluctuation)" Trans.JSME. 58-551. 2087-2092 (1992)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] T.Fukano: "Periodic Velocity Fluctuation in the Near Wake of a Rotating Flat-Blade and its Roll in the Generation of Turbulent Noise" ACOUSTIC EFFECTS IN FSI(ASME WAM). 4. 1-14 (1992)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] H.Hayashi: "An Experimental Investigation on the Discrete Frequency Noise Generated from a NACA blade Immersed in a Uniform Flow" Trans.JSME.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] T.Fukano: "Estimation of Spectrum Distribution of Broad Band Noise Generated from a Rotating Flat-Plate blade" Trans.JSME.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1992 Final Research Report Summary
  • [Publications] 深野 徹,福原 稔,松尾 哲,林 秀千人: "回転する単独平板翼の後流に関する研究(第2報,迎え角が小さい場合の流動様相に与える先端すきまの影響)" 日本機械学会論文集(B編). 57-535. 891-897 (1991)

    • Related Report
      1992 Annual Research Report
  • [Publications] 深野 徹,福原 稔,磯部 浩,広中 康生,林 秀千人: "回転する単独平板翼の後流に関する研究(第3報,速度の周期変動現象に及ぼす後縁形状の影響)" 日本機械学会論文集(B編). 58-551. 2087-2092 (1992)

    • Related Report
      1992 Annual Research Report
  • [Publications] Fukano,T.,Hayashi,H.,Isobe,H.,Hironaka,Y.& Fukuhara.M..: "Periodic Velocity Fluctuation in the Near Wake of a Rotating Flat-Plate Blade and its Roll in the Generation of Turbulent Noise" ACOUSTICAL EFFECTS IN FSI (ASME WAM). 4. 1-14 (1992)

    • Related Report
      1992 Annual Research Report
  • [Publications] 林 秀千人,深野 徹: "一様流中のNACA対称翼から発生する離散周波数騒音に関する実験的研究(翼厚による発生機構の差異)" 日本機械学会論文集(B編).

    • Related Report
      1992 Annual Research Report
  • [Publications] 深野 徹,濱川 洋充,林 秀千人,猿渡 博孝: "回転する単独平板翼から発生する広帯域騒音のスペクトル密度分布の予測に関する研究" 日本機械学会論文集(B編).

    • Related Report
      1992 Annual Research Report
  • [Publications] 深野 徹,福原 稔,松尾 哲,林 秀千人: "回転する単独平板翼の後流に関する研究(第2報,迎え角が小さい場合の流動様相に与える先端すきまの影響)" 日本機械学会論文集(B編). 57ー535. 891-897 (1991)

    • Related Report
      1991 Annual Research Report
  • [Publications] 深野 徹,福原 稔,磯部 浩,広中 康生,林 秀千人: "回転する単独平板翼の後流に関する研究(第3報,速度の周期変動現象に及ぼす後縁形状の影響)" 日本機械学会論文集(B編).

    • Related Report
      1991 Annual Research Report
  • [Publications] Fukano,T.,Hayashi,H.,Isobe,H.,Hironaka,Y.& Fukuhara,M..: "Periodic Velocity Fluctuation in the Near Wake of a Rotating FlatーPlate Blade and its Roll in the Generation of Turbulent Noise" 1992年ASME SIMPOSIUM ON FLOWーINDUCED VIBRATION AND NOISE.

    • Related Report
      1991 Annual Research Report

URL: 

Published: 1991-04-01   Modified: 2016-04-21  

Information User Guide FAQ News Terms of Use Attribution of KAKENHI

Powered by NII kakenhi