机械
雷诺数
涡轮机
阻力
Lift(数据挖掘)
转子(电动)
米
扭矩
入口
流量测量
雷诺平均Navier-Stokes方程
升阻比
涡轮叶片
海洋工程
工程类
物理
机械工程
计算流体力学
湍流
计算机科学
数据挖掘
天文
热力学
作者
R. E. Thompson,Jerry Grey
出处
期刊:Journal of Basic Engineering
[ASME International]
日期:1970-12-01
卷期号:92 (4): 712-722
被引量:42
摘要
A theoretical model of a turbine meter operating in the high Reynolds number regime has been formulated to study the effects of retarding torques, inlet velocity profile, blade interference effects, meter geometry, and other factors. A computer program predicts actual rotor speed by numerical integration of the lift and drag forces on the rotor blade. Numerical sample calculations indicated substantial effects due to velocity profile and blade interference. Retarding torques were relatively unimportant in the high Reynolds number range.
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