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- Vortices of nozzle exit and whistle exit move gradually towards the downstream and spread outside under the action of potential flow field and other vortices. 在喷嘴出口与哨嘴出口处形成的旋涡结构,在势流流场和其它涡元的作用下逐渐向下游运动,并向两边扩散。
- Equivalent potential flow numerical method for the flow field 流场数值计算的等效势流法
- Approximate Solution to Potential Flow Field for Axially Symmetric Bodies 轴对称物体势流场的近似解
- The teeming time and height affect flow field too. 并分析了流体注入时间、注入高度对流场的影响。
- Pipe flowmeter is a very potential flow metering equipment. 弯管流量计是一种有潜力的流量计量仪器。
- Such as: the balance of elastic membrane, the heat conduction of stationary state, the incompressible potential flow, the problem of electrostatic field and magnetostatics field. 弹性膜的平衡问题,稳定状态的热传导问题,不可压缩势流问题,静电场问题以及静磁场问题。
- Error: gui-monitor-residuals: Uninitialized flow field. 直译就是流场没有初始化!!!!重新初始化。
- Fluid pressure signal validates result of flow field computation. 液体压力信号验证流场建模与计算的结果。
- In order to develop the predictable and quantitative research technology, the potential flow theory was used to simulate the bottom?hole crossflow field. 而喷嘴几何形状、喷嘴布置方式是决定井底漫流场是否合理的关键因素。
- The research was made on the afterbody flow field of civil aircraft. 本文运用计算与实验相结合的研究方法对民机机身后体流场进行了研究。
- The position of the bottom blown nozzles will influence the flow field d... 在吹气量一定的情况下,底吹喷嘴位置对流场有较大影响。
- The typical seepage flow field of the bottom for the spillway dam is obtai... 最后计算了典型的坝基渗流流场,计算结果与实验结果吻合较好。
- Experimental Study on Image Preprocessing of Thermal Flow Field Tomogram[J]. 引用该论文 姚卫;闫大鹏;王振东;尤海航;贺安之.
- The potential flow theory is then applied to the overlap of the slipstream and the flow over the wing. 用位流理论来处理螺旋桨滑流与机翼绕流的迭加。
- The second part is about the airfoil analysis and design of two-dimensional inviscid incompressible potential flow. 第二部分是二维无粘不可压势流的 翼型分析和设计问题。
- The aerodynamic force is solved with the second order approximation method for transonic small disturbance potential flow. 用跨音速小扰动势流的二级近似方法求解气动力;
- Making use of these results, we obtained an exact solution for the incompressible potential flow through a two-dimensional Laval nozzle. 利用这些结果得到了二元拉伐尔喷管内不可压缩位势流动的精确解。
- Finally, experiments are performed to testify the flow field simulation results of FTX polygon. 最后本文对六棱柱元件的流场模拟计算结果进行了实验验证。
- This curvature of the flow field alters the pressure distribution and the aerodynamic forces from their values in translational flight. 流场的弯曲使压力分布和空气动力与直线飞行时的值相比发生了变化。
- When wave breaking occurs,strong eddies appears, and the flow around the breakwater cannot be described withpure potential flow theory. 为方便开边界的处理,采用了在计算域中添加源项的方法造波。