离散涡的英文

• discrete vortex

• "离散"英文翻译    dispersed; scattered about; ...
• "涡"英文翻译    eddy; whirlpool; vortex
• "离散涡元" 英文翻译 :    discrete vortex elements
• "扩散涡管" 英文翻译 :    diffusing scroll
• "离散" 英文翻译 :    dispersed; scattered about; separated from one another; spread; debunching; straggling; fringing; straddling; variance 骨肉离散。 the family were scattered in different places
• "非离散" 英文翻译 :    non discrete; nondiscrete
• "共离散" 英文翻译 :    covariance
• "角离散" 英文翻译 :    angle straggling
• "离差；离散" 英文翻译 :    dispersion
• "离散斑" 英文翻译 :    discrete spot
• "离散带" 英文翻译 :    divergent belt; divergent zone
• "离散的" 英文翻译 :    discrete; stray
• "离散点" 英文翻译 :    discrete points
• "离散度" 英文翻译 :    degree of dispersion; degree of separation; dispersion
• "离散化" 英文翻译 :    discretize; diskretisierung discretization; iscretization
• "离散集" 英文翻译 :    discrete set; isolated set
• "离散角" 英文翻译 :    walk off angle; walk-off angle
• "离散解" 英文翻译 :    discrete solution
• "离散力" 英文翻译 :    dispersive kraeft edispersive forces
• "离散量" 英文翻译 :    discrete magnitude
• "离散流" 英文翻译 :    discrete flow
• "离散码" 英文翻译 :    discrete code
• "离散模" 英文翻译 :    walk-off-mode
• "离散谱" 英文翻译 :    discrete spectrum; point spectrum
• "离散区" 英文翻译 :    scattering zone

• 5 . the numerical simulation of the axial vortex movement in the inlet side of the pump system with the method of discrete vortex provided a new way for hydromechanical characteristics of a pump system
  用离散涡方法计算涡系位置的演化模拟泵入口侧涡量场的轴向涡流运动，为研究泵系统入流侧涡量场特性提供了一种定量研究方法。
• The transient continuously distributive vortex can be replaced by a number of discrete point vortexes . the trajectory of vortex movement was computed with the method of discrete vortex and the axial vortex movement in the inlet side of the pump system was simulated
  将泵入口侧连续分布的涡量场离散成有限数目的离散涡，用离散涡方法计算涡系位置的演化，模拟泵入口涡量场的轴向涡流运动。
• Based on the green ' s formula and the assumption of the propeller blade ' s thin sections , a lifting - surface method of propellers with the vortex lattice and equal source panel distributions on the mean camber surface has been introduced for the prediction of steady propeller ' s hydrodynamics in this paper . an approximate kurta condition was applied
  基于creen公式和薄翼理论假设导出的升力面方法，采用在螺旋桨拱弧面上分布离散涡、源布置方法预报均匀流场中的螺旋桨的定常性能，螺旋桨尾涡面上压力连续性条件采用近似的kutta条件处理。