片语

Note on Unsteady Boundary-Layer Separation的翻译是关于不平稳的界限层数分离的笔记

turbulent boundary layer separation紊流边界层分离

boundary layer separation point边界层分离点

laminar boundary layer separation层流边界层分离

boundary layer separation loss附面层脱离损失

boundary layer separation theory边界层分离理论

boundary y layer separation边界层分离

英汉例句

• The technology of oil flow and silk thread can reflect effect of the vertex generators controlling the boundary layer separation of the wing truly.

  油流和丝线流动显示技术可真实反映涡流发生器对机翼附面层分离的控制效果。

• The boundary layer separation points, minimum pressure positions on the surface and the drag coefficients are in agreement with numerical solutions and experimental results.

  边界层分离点、物面最小压力点及阻力系数的计算结果与一些数值解及实验结果是符合的。

• Finally recent studies of turbulent boundary layer separation are also briefly reviewed.

  最后简单介绍了目前在研究湍流边界层分离方面的进展。

• According to the analysis on the boundary layer separation condition, parameter equation of vane curve for centrifugal pump is established.

  通过对压力面边界层分离条件的分析得出叶片型线方程并给出计算实例。

• Based on linear wave making resistance theory and on & technique of boundary layer separation control, the present paper gives an optimized study of hull form below the design water line.

  本文基于线性兴波阻力理论，把控制尾流分离作为约束条件，利用优化计算方法对设计水线下船体外形进行优化研究。

• The introduction of micro pressure sensor array expands ways detecting boundary layer separation point.

  微型压力传感器阵列的引入，拓宽了边界层分离点检测的解决途径。

• If the reference separation point approaches the outlet, the test results are satisfactory, which state that the practical position of boundary layer separation point will be close to the outlet.

  若分离参考点接近于出口端，则可获得满意的测试结果，这说明边界层实际分离点的位置已经很接近于叶片的出口端。

• The theoretical analysis and experimental results show that boundary layer separation will produce pressure drag.

  理论分析和实验的结果说明：边界层分离将引起压差阻力。

• The basic equations of the boundary layer for blade surface flow of arbitrary cyclical surface are established, and the rotating effect for boundary layer separation is analyzed.

  建立任意廻转面叶片表面边界层基本方程组，分析边界层分离的旋转效应。