来流速度的英文

例句与用法

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1. The vortex - vibration was measured when the towed velocity , dip angle between the circular cylider and flow velocity , and diameter were varied
   对不同拖曳速度、拖缆倾角，即拖缆与来流速度之间的夹角和不同直径的拖缆涡激振动进行了测量分析。
2. A cascaded architecture is adopted , where desired propeller rate of revolution is generated by solving a static 2nd order equation with a parameter of desired thrust force , which is the input of the speed / position tracking control
   在推进器动态模型的基础上，采用滑模控制的方法，由速度位置误差获得期望推力，再通过求解包括来流速度的二次方程得到期望螺旋桨转速。
3. At large attack angle the frequency of the vortex has n ' t a apparent zone of " lock - in " . the fluid - induced vibration at large attack angle belongs to the stable dynamic response problems . but a sudden skip of amplitude will occur at large inlet velocity
   在大攻角下分离涡脱落的频率没有一个明显的频率锁定区域，流体振动属于稳定的动力响应问题，但在大来流速度下会出现振幅突跳的现象。
4. The influence of inflow velocity , the baffle body height and the clapboard position on the flow velocity , flow equilibrium between the two sides of the clapboard , particle distribution , rich / lean concentration ratio and flow resistance characteristic are studied numerically
   文章研究了来流速度，撞击块高度、隔板位置等因素对气相速度场、隔板两侧配风均匀性、颗粒浓度、浓淡分离比和燃烧器内阻力特性的影响。
5. Results show that the influence of mainstream reynolds numbers on heat transfer coefficience is little and the heat transfer coefficience raise with the increase of reynolds numbers . the influence of the position of holes on heat transfer coefficience is complex and correlate with the mainstream speed and the balde surface curvature . and the influence of blowing ratio on heat transfer coefficience is more great ( especially to stator ) , and show a complex relation to mainstream reynolds number and the position of holes
   实验结果表明，不同孔位出流的换热由于孔排下游表面来流速度及叶片表面曲率的不同而有不同的规律，而主流雷诺数对叶片表面特别是压力面和前缘区域的换热系数比的影响较小，吹风比对换热系数影响较大(特别是导叶) ，并且随气膜孔位置和来流雷诺数的变化而情况复杂。