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Active Control of Cascade Flutter in High-speed Flows by Acoustic Excitation

Research Project

Project/Area Number 09450371
Research Category

Grant-in-Aid for Scientific Research (B)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionKYUSHU UNIVERSITY

Principal Investigator

TOSHIMITSU Kazuhiko  Facylty of Engineering, KYUSHU UNIVERSITY,Research Associate, 工学部, 助手 (10180150)

Co-Investigator(Kenkyū-buntansha) INOKUCHI Yuzo  Faculty of Engineering, KYUSHU UNIVERSITY,Research Associate, 工学部, 助手 (30274509)
YAMASSAKI Nobuhiko  Faculty of Engineering, KYUSHU UNIVERSITY,Associate Professor, 工学部, 助教授 (70166635)
NAMBA Masanobu  Faculty of Engineering, KYUSHU UNIVERSITY,Professor, 工学部, 教授 (50037735)
Project Period (FY) 1997 – 1998
Project Status Completed (Fiscal Year 1998)
Budget Amount *help
¥13,600,000 (Direct Cost: ¥13,600,000)
Fiscal Year 1998: ¥1,300,000 (Direct Cost: ¥1,300,000)
Fiscal Year 1997: ¥12,300,000 (Direct Cost: ¥12,300,000)
KeywordsFlutter / Cascade / PIV / Sound wave / Active control / Velocity vector / Unsteady flow
Research Abstract

New subsonic wind tunnel facility for active control of cascade flutter and particle image velocimetry (PIV) has been constructed. Using the system and numerical simulations, the following results are obtained.
Active Control :
・ Flutter frequency and critical velocity of a flat plate blade (139.5*50*1mm) are estimated 118 Hz and 143 m/s respectively from the flutter experiment. On the other hand, they are found to be 165Hz and 123m/s from a finite element method calculation. This is because the FEM calculation neglects the effect of separated flow on the surface of a blade vibrating.
・ The optimum suppression conditions of the flutter are calculated as follows ;
- The center of actuator is located at the center of chord in stream-wise direction,
- The amplitude and phase difference are 0.14 and -54 degrees respectively, which are normalized by bending oscillation.
・ Amplitude of blade vibration is decreased by the acoustic excitation from two actuator diaphragms on tip-side wall when the diaphragms are operated based on bending vibration of the blade.
PIV :
・ Uniform flow velocity vectors are measured with the PIV system.
・ Velocity vectors of steady flow around biconvex blade are measured with the PIV system.
・ Turbulent flow around cylinder at Reynolds Number 1.0x10^5 is visualized with the NV system, in particular K・rm・n vortices behind cylinder are periodically observed.

Report

(3 results)
  • 1998 Annual Research Report   Final Research Report Summary
  • 1997 Annual Research Report
  • Research Products

    (6 results)

All Other

All Publications (6 results)

  • [Publications] 利光和彦,他3名: "音波による低周波数翼フラッタの能動的抑止" 九州大学工学集報. 72・2. 109-114 (1999)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1998 Final Research Report Summary
  • [Publications] 利光和彦,他3名: "音波による低周波数翼列フラッタの能動的抑止" 九州大学工学集報. 72・2. 115-121 (1999)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1998 Final Research Report Summary
  • [Publications] Kazu Toshimitsu, Takeshi Otsuka, Hiroko Maruo and Masanobu Namba: "Active Control of Low Frequency Blade Flutter by Acoustic Excitation" Technology Reports of Kyushu University. 72-2. 109-114 (1999)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1998 Final Research Report Summary
  • [Publications] Kazu Toshimitsu, Akihiro Yamagata, Kenichiro Nagai and Masanobu Namba: "Active Control of Low Frequency Cascade Flutter by Acoustic Exciation" Technology Reports of Kyushu University. 72-2. 115-121 (1999)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1998 Final Research Report Summary
  • [Publications] 利光和彦,他3名: "音波による低周波数翼フラッタの能動抑止" 九州大学工学集報. 72・2. 109-114 (1999)

    • Related Report
      1998 Annual Research Report
  • [Publications] 利光和彦,他3名: "音波による低周波数翼列フラッタの能動的抑止" 九州大学工学集報. 72・2. 115-121 (1999)

    • Related Report
      1998 Annual Research Report

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Published: 1997-04-01   Modified: 2016-04-21  

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