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Charts of Additive Drag Coefficient and Mass-Flow Ratio for Inlets Utilizing Right Circular Cones at Zero Angle of Attack

机译：零攻角下利用右圆锥进气道的附加阻力系数和质量流量比图

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作者
Mascitti, V. R.;
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年度 1966
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
Chart ; Conical inlet ; Drag coefficient ; Mass flow ; Additive ; Angle of attack ; Calculation ; Coefficient ; Cone ; Drag ; Flow ; Hypersonic ; Inlet ; Mach number ; Mass ; Sonic ; Supersonic;

机译：图表;锥形入口;阻力系数;质量流量;添加剂;迎角;计算;系数;锥;阻力;流量;高超音速;进口;马赫数;质量;声波;超音速;

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1. A computational study of the effect of angles of attack on a double-cone type supersonic inlet with a bleeding system [J] . Kyung Jin Ryu, Seol Lim, Dong Joo Song Computers & Fluids . 2011,第1期

机译：攻角对带泄漏系统的双锥型超声速进气道影响的计算研究
2. Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack [J] . 刘建新, 罗纪生应用数学和力学：英文版 . 2010,第005期

机译：入口扰动对小迎角钝锥上高超声速边界层过渡的影响
3. Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack [J] . Jian-xin LIU, Ji-sheng LUO 应用数学和力学（英文版） . 2010,第005期

机译：入口扰动对小迎角钝锥上高超声速边界层过渡的影响
4. Effect of Inlet Slot Number on the Spray Cone Angle and Discharge Coefficient of Swirl Atomizer [C] . Mohd Syazwan Firdaus Mat Rashid, Ahmad Hussein Abdul Hamid, Ow Chee Sheng, International Symposium on Robotics and Intelligent Sensors . 2012

机译：入口槽数对旋流雾化器喷雾锥角和放电系数的影响
5. Hypersonic crossflow instability and transition on a circular cone at angle of attack. [D] . Ward, Christopher A. C. 2010

机译：高音速横流失稳和在迎角处的圆锥上过渡。
6. Drag force as a function of cross section and angle of attack. A hydraulic laboratory dataset for numerical validation [O] . Cian J. Desmond, Florent Thiebaut, Jimmy Murphy 2019

机译：阻力与横截面和攻角的关系。用于数值验证的液压实验室数据集
7. 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。
8. Charts of additive drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack [R] . Mascitti, V. R. 1966

机译：添加剂阻力系数和质量流量比的图表在零迎角时利用右圆锥的入口

Charts of Additive Drag Coefficient and Mass-Flow Ratio for Inlets Utilizing Right Circular Cones at Zero Angle of Attack

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