| Project/Area Number |
09450371
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | KYUSHU UNIVERSITY |
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Principal Investigator |
TOSHIMITSU Kazuhiko Facylty of Engineering, KYUSHU UNIVERSITY,Research Associate, 工学部, 助手 (10180150)
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| 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)
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| Project Period (FY) |
1997 – 1998
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| Project Status |
Completed (Fiscal Year 1998)
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| 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)
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| Keywords | Flutter / Cascade / PIV / Sound wave / Active control / Velocity vector / Unsteady flow |
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| 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.
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