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Effect of Boattail Angle on Pressure Distribution and Drag of Axisymmetric Afterbodies under Low-Speed Conditions

机译：BOATTAIL角对低速条件下压力分布与轴对称后透明度的影响

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The Hung TRAN; Takumi AMBO; Lin CHEN; Taku NONOMURA; Keisuke ASAI;
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1. The Effect of Boattail Angles on the Near-Wake Structure of Axisymmetric Afterbody Models at Low-Speed Condition [J] . The Hung Tran International journal of aerospace engineering . 2020,第4期

机译：Boattail角度在低速条件下轴对称轴对称模型近尾结构的影响
2. Effect of boattail angles on the flow pattern on an axisymmetric afterbody surface at low speed [J] . Tran The Hung, Ambo Takumi, Lee Taekjin, Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics . 2018,第期

机译：Boattail角度在低速下轴对称轴对称的流动模式的影响
3. APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - Flow behavior at different boattail angles of an axisymmetric body in low-speed regime. [J] . Tran The Hung, Takumi Ambo, Taekjin Lee, Bulletin of the American Physical Society . 2017,第14期

机译：APS-APS流体动力学分部第70届年会-事件-低速状态下轴对称物体的不同船尾角处的流动行为。
4. DRAG PREDICTION FOR SUPERSONIC CIVIL TRANSPORT AIRCRAFT AT LOW-SPEED, TRANSONIC AND SUPERSONIC CONDITIONS [C] . Gerald Carrier, Daniel Destarac CEAS Aerospace Aerodynamics Research Conference . 2002

机译：以低速，跨音速和超声波条件拖曳超音速民用运输机的预测
5. Experimental study on the effects of nose geometry on drag over axisymmetric bodies in supersonic flow. [D] . Brooker, B. Tyler. 2014

机译：鼻子几何形状对超声速流中轴对称物体上阻力的影响的实验研究。
6. Association of quadriceps angle with plantar pressure distribution navicular height and calcaneo-tibial angle [O] . Ata Elvan, Ibrahim Engin Simsek, Mehmet Alphan Cakiroglu, 2019

机译：股四头肌角与足底压力分布鼻高和胫腓骨角的关系
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. DONBOL: A Computer Program for Predicting Axisymmetric Nozzle Afterbody Pressure Distributions and Drag at Subsonic Speeds [R] . Putnam, L. E. 1979

机译：DONBOL：用于预测轴对称喷嘴后体压力分布和亚音速速度阻力的计算机程序

Effect of Boattail Angle on Pressure Distribution and Drag of Axisymmetric Afterbodies under Low-Speed Conditions

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