STUDY OF 3-DIMENSIONAL INTERTACTINS BETWEEN WAKE VORTICES AND FLOWS NEAR SEPARATION LINES
STUDY OF 3-DIMENSIONAL INTERTACTINS BETWEEN WAKE VORTICES AND FLOWS NEAR SEPARATION LINES
批准号:
10650895
负责人:
NISHIKAWA Nobuhide
金额:
$2.24万
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:
1998
资助国家:
日本
项目状态:
已结题
起止时间:
1998 至 2000
中文摘要
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英文摘要
Three dimensional separated flow over axisymmetric paraboloid at incidence angles ; α=30, 40 and 50 deg has been investigated by three approaches such as particle image velocimetry, numerical study. and measurement with constant temperature anemometer.Partcle image velocimetry : Supplying tracers with a fog machine or plastic balloons. Laser light sheet is used in studying the structure of the vortices in cross-sections of flow, for which two-color Laser dual sweep has been employed. The user-friendly PIV technique has been developed with separating Argon laser beam into Blue and Green by dichroic mirror, and the flow reversal can be detected. Velocimetry results at α=30, or 40 deg shows at most 20% deviation from the following anemometer results, where Reynolds numbers is 9000 referred to the base diameter.Numerical simulation : The attempt of numerical simulation of the flow is performed with a pseudo-compressibility method with Beam and Warming method . The results are compared with … More the anemometry experiment. and it was realized that the prediction is good for the 40deg and 50 deg cases where strong vortices appear.Hot wire anemometry. The flow at the same condition as in PIV study has been investigated experimentally with a hot wire anemometer. Reynolds numbers are 9.0×10^3 and 1.8×10^4 referred to the base diameter. X-type probe has been used to measure three dimensional velocity fields. Velocity fluctuations at sampling time of 4kHz have been also evaluated. The output signals show the change of R.M.S.value and Reynolds stress in various cross-sections and that the spatial correlation factors are small at the locations of large R.M.S.value. Laser light sheet method is used in studying the structure of the vortices in separated flow. The development of lateral vortices in each cross-section of the body is visualized. The variation of vortex patterns is shown for each cross-section, angle of attack and Reynolds number. With both results of anemometry and visualization, it has been confirmed that at large αsuch as 50 deg, the leeside vortex interacts unsteadily with the velocity fluctuations in the wake behind the body. Less
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T.ISHIDE, N.NISHIKAWA and F.MIKAMI: "Clarification of Unsteady Characteristics in Separated Flow over a Axisymmetric Parboloid at High Angle of Attack (in Japanese)"J.Japan Soc.Aeron.Space Sciences. Vol.48, No.562. 377-384 (2000)
T.ISHIDE、N.NISHIKAWA 和 F.MIKAMI:“高攻角轴对称抛物面分离流不稳定特性的澄清(日文)”J.Japan Soc.Aeron.Space Sciences。
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西川進栄,石出忠輝,三神史彦: "軸対称物体まわりの剥離流の実験と画像速度計測の動向(総説)"日本航空宇宙学会誌、. Vol.48,No.561. 543-548 (2000)
Shinei Nishikawa、Tadateru Ishide、Fumihiko Mikami:“轴对称物体周围分离流的实验和图像速度测量的趋势(评论)”日本航空学会杂志,第 48 卷,第 561 期。543-548(2000 年) )
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T.ISHIDE,N.NISHIKAWA and F.MIKAMI,: "Experimental Investigation of Three-Dimensional Separated Flow over Body of Revolution at High Angle of Attack,"Proceedingsof of 22nd International Congress of Aeronautical Science. 2-9-6 (2000)
T.ISHIDE、N.NISHIKAWA 和 F.MIKAMI,“高迎角回转体上三维分离流的实验研究”,第 22 届国际航空科学大会论文集。
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石出忠輝、西川進栄、三神史彦: "三次元境界層剥離の可視化と熱線計測"航空宇宙学会論文集、. 48巻553号. 27-33 (2000)
Tadateru Ishide、Shieikawa、Fumihiko Mikami:“三维边界层分离和热射线测量的可视化”日本航空学会学报,第 48 卷,第 553 期。27-33(2000 年)
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共 7 条
Study of Separated flow over bodies at high incidence with towing in air-filed chamber
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批准号:20560734
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$3.0万
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财政年份:2008
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负责人:NISHIKAWA Nobuhide
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依托单位:
Fluctuation Distribution and Vortex Structure of in Three Dimensional Separated Flow
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批准号:03650049
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.34万
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财政年份:1991
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负责人:NISHIKAWA Nobuhide
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依托单位:
Experiment and Nemerical Prediction for Onset of od Three Diemnsional Separation
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批准号:61550042
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.15万
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财政年份:1986
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负责人:NISHIKAWA Nobuhide
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依托单位:
海外基金