• 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。

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  • The negative bowed blades raise the endwall loading and emphasis the boundary layer separation.

    叶片反弯增加了端区叶片的负荷,加重了附面层的分离。

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  • The control of supercritical airfoil boundary layer separation is adapted using micro-vortex generators.

    超临界翼型附面层分离控制适合采用微型涡流发生器。

    youdao

  • Thin-layer separation, color and quantitation method for the analysis of chloroacetamide herbicides was studied.

    本文研究了氯代乙酰胺类除草剂的薄层分离、显色和定量方法。

    youdao

  • 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。

    youdao

  • This paper presents the effect of different heat treatments on performance of new low layer separation valve steel LF6.

    研究了不同热处理制度对一种新型的低层状析出气阀钢LF6性能的影响。

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  • 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。

    youdao

  • 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。

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  • 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。

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  • 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。

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  • 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。

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  • This design proposal of micro pressure sensor array can effectively meeting the measuring requirement of boundary - layer separation point, and expand engineering applied scope of MEMS devices.

    设计的微型压力传感器阵列可有效满足边界层分离点的检测要求,进一步拓展了MEMS器件的工程应用范围。

    youdao

  • 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。

    youdao

  • 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。

    youdao

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