| 1. | Subsonic potential flow
亚声速势流 |
| 2. | Acyclic potential flow
无环量势流 |
| 3. | 2d potential flow
二维势流 |
| 4. | 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。 |
| 5. | Calculation of the potential flow around a submerged body is an important problem in applications
水面下物体的绕流问题是一个有着重要应用背景的问题。 |
| 6. | Firstly , fkdv equation for the nonlinear surface wave was obtained by perturbation technique from potential flow theory
首先，从势流理论出发，利用摄动法，导出了非线性表面波遵循的fkdv方程。 |
| 7. | Under the assumptions of linearized potential flow , the coupled problem of flow in the interior and exterior fluid regions is solved by an eingenfunction - expansion approach
在线性有势流的假定下，用特征函数展开方法求出了内部和外部流场的解。 |
| 8. | Parameters influencing aerodynamic flows and transition and influence of boundary layers on outer potential flow are presented , along with associated stall and drag mechanisms
而边界层理论受限于各种流体种类的假设，像是可压缩性、紊流、维度和热传。 |
| 9. | 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
例如：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。 |
| 10. | With panel method and finite difference method , the matching of flow parameters on the boundary between viscous and potential flow can be carried out for the two - phase flow on blade surface
本文以naca4412和naca0012两种翼型为例，通过压力分布计算以及同试验数据的比较分析表明，面元法可以给出更高的精度。 |
