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Determination of the Aerodynamic Drag Force on a Parachute

机译:降落伞上气动阻力的测定

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摘要

The use of the Buckingham Pi theorem in dimensional analysis suggests that the aerodynamic drag force that is exerted on parachutes is a quadratic function of speed, but it cannot determine the drag coefficients because they must be determined experimentally. In this article, experimental data are presented and used in two different, but complementary, ways to demonstrate that the drag force is quadratic, and to determine the corresponding drag coefficients. Curve-fitting a second-degree polynomial to the collected data makes it possible to verify directly that the nature of the force is quadratic and to estimate drag coefficients. Predicted terminal speeds of the parachutes are also used to determine the drag coefficients. A comparison of the two sets of results indicates that the combined use of the methods helps improve the accuracy of the drag force obtained.
机译:在尺寸分析中使用白金汉Pi定理表明,降落伞上施加的空气动力阻力是速度的二次函数,但无法确定阻力系数,因为它们必须通过实验确定。本文以两种不同但互补的方式介绍并使用了实验数据,以证明阻力是二次方的,并确定相应的阻力系数。将二阶多项式曲线拟合到所收集的数据使得可以直接验证力的性质是否为二次方并估计阻力系数。降落伞的预测终端速度也用于确定阻力系数。两组结果的比较表明,这些方法的组合使用有助于提高获得的阻力的准确性。

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    Njock Libii Josué;

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  • 年度 2007
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