• The aerodynamic drag of different models at zero angle of attack in the experiment is calculated using the simplified procedure.

    在零攻角实验时不同模型的空气动力阻力是采用简化方法来计算的;

    youdao

  • In ocean engineering realm, fluid drags are computed by Morison equation with drag coefficient defined by a function of Renold number and attack Angle.

    在海洋工程领域,计算软管流体阻力采用莫里逊公式,其中阻力系数是双参数迎角和雷诺数的函数。

    youdao

  • The aerodynamic drag and lift of javelin increase with angle of attack.

    标枪的气动阻力、升力随迎角增加而增加。

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  • This paper introduces a process method of the pressure data in the wake to obtain the drag characteristics with high accuracy, and discusses about the drag measurement at high Angle of attack.

    本文就如何处理尾迹区的测压数据来确保阻力测量的精确度及如何测出大迎角的阻力特性进行了一些探讨。

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  • The change rules of aerodynamic parameters including lift coefficient, drag coefficient and pitch moment coefficient have been analyzed when Angle of attack and fuel flow rate is changed.

    考虑了不同飞行攻角、不同燃料流率下气动参数,包括升力系数、阻力系数和俯仰力矩系数的变化规律。

    youdao

  • It is found that the variation of planforms and geometrical parameters can effect only the drag reduction but little to the low lift in low angle of attack condition.

    发现单纯改变涡襟翼的形式和参数能提高减阻效果,但不能改变小迎角下升力过小的现象。

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  • According to the data given by the Weibull radar, the drag coefficient and angle of attack were identified.

    提出了利用韦布尔雷达测量的速度及弹道参数来辨识非常规弹丸飞行的阻力系数和攻角的方法。

    youdao

  • According to the data given by the Weibull radar, the drag coefficient and angle of attack were identified.

    提出了利用韦布尔雷达测量的速度及弹道参数来辨识非常规弹丸飞行的阻力系数和攻角的方法。

    youdao

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