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Flow Patterns and Pressure Distributions around a Bluff Afterbody in the Wake of a 120 Deg Cone for Various Separation Distances at Mach 3.0

机译：绕过Bluff后体的流动模式和压力分布在120度锥体的尾流中，以3.0马赫的速度进行各种分离距离

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作者
Deveikis, W. D.; Sawyer, J. W.;
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年度 1971
页码 1-4
总页数 4
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Ballutes ; Flow distribution ; Pressure distribution ; Wind tunnel models ; Afterbodies ; Conical bodies ; Flow visualization ; Reynolds number ; Wakes;

机译：Ballutes;流量分布;压力分布;风洞模型;后体;锥体;流动可视化;雷诺数;尾流;

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专利

1. Cold-flow patterns behind novel rifled bluff-body cones [J] . Kuo C. San, Chih L. Shih, Shun C. Yen Journal of Mechanical Science and Technology . 2014,第3期

机译：新型线状钝体锥体后面的冷流模式
2. Separation delay through contoured transverse grooves on a 2D boat-tailed bluff body: Effects on drag reduction and wake flow features [J] . Mariotti A., Buresti G., Salvetti M. V. European Journal of Mechanics, B. Fluids . 2019,第期

机译：通过轮廓横向凹槽的分离延迟在2D船尾的凹槽体上：对减阻和唤醒流动特征的影响
3. FLOW SEPARATION, WAKE VORTICES AND PRESSURE DISTRIBUTION AROUND A CIRCULAR CYLINDER UNDER OSCILLATORY WAVES [J] . Hajime Ishida, Yuichi Iwagaki Proceedings of the International Conference on Coastal Engineering . 1976,第15期

机译：振荡波作用下圆圆柱周围的流动分离，尾迹和压力分布
4. Boundary-layer Separation Detection for a Cone at High Angle of Attack in Mach 4.5 Flow with Pressure-Sensitive Paint [C] . Carson L. Running, Michael J. Thompson, Thomas J. Juliano, AIAA Fluid Dynamics Conference;AIAA Aviation Forum . 2017

机译：压力敏感涂料在4.5马赫流动中高攻角锥的边界层分离检测
5. Turbulence effects on the flow and pressure distributions around three-dimensional bluff bodies. [D] . Sitheeq, Mohamed K. 1997

机译：湍流对三维钝体周围流动和压力分布的影响。
6. Measurements of the pressure distributions on two circular cylinders of diameter d, vertically immersed in a turbulent boundary layer, are performed for various cylinder spacings s and angles of attack φ. The characteristics of the drag and lift forces acting on the cylinder are classified into three regions : i.e., 1) 0°＜__〜φ＜__〜30°, 2) 30°＜__〜φ＜__〜120°and 3) 120°＜__〜φ＜__〜180°which are divided by the two zero-lift force lines. Moreover, it is found that the interference between two cylinders is almost negligible for s/d＞__〜4, except for the influence of the wake region of the upstream cylinder. [O] . 谷口清一, 坂本弘志, Seiichi TANIGUCHI, 1980

机译：对于不同的气缸间距s和迎角φ，对垂直浸入湍流边界层的直径为d的两个圆柱上的压力分布进行测量。作用在气缸上的阻力和提升力的特性分为三个区域：1）0°＜__ 〜φ ＜__ 〜30°，2）30°＜__ 〜φ ＜__ 〜120°和3） 120°＜__ 〜φ ＜__ 〜180°除以两条零升力线。而且，发现除了上游气缸的尾流区域的影响之外，对于s / d＞ __〜4，两个气缸之间的干扰几乎可以忽略。
7. Flow patterns and pressure distributions around a bluff afterbody in the wake of a 120 deg cone for various separation distances at Mach 3.0 [R] . Deveikis, W. D., Sawyer, J. W. 1971

机译：在120度锥体尾部的虚张声势后体周围的流动模式和压力分布，以3.0马赫的速度进行各种间隔距离

Flow Patterns and Pressure Distributions around a Bluff Afterbody in the Wake of a 120 Deg Cone for Various Separation Distances at Mach 3.0

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