超声速翼型气动特性研究

Wen-Liang Yong
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引用次数: 2

摘要

随着飞机的发明,它变得比最初的莱特兄弟飞机更快、更大。当速度高到足以跨越音速时,由于冲击波的存在,空气条件将与低速时不同。在这项工作中,我们介绍了几种数值方法来分析当速度高于声速时翼型的性能。利用这些数值方法,我们分析了菱形翼型在不同攻角和速度下的性能。有了这些数据,工程师可以在设计高速飞机时选择更好的翼型,以获得更低的阻力系数和升力系数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on Aerodynamic Characteristics of Supersonic Airfoil
With the invention of the aircraft, it has become much faster and larger than the original Wright Brothers aircraft. When the speed is high enough to cross the speed of sound, air conditions will be different than that in low speed due to the existence of shock wave. In this work, we introduce several numerical ways to analyze the performance of the airfoil when the speed is higher than the speed of sound. With these numerical methods, we analyzed the performance of diamond-shaped airfoil under different angles of attack and speed. With this data, engineers can choose a better airfoil to attain a lower drag coefficient as well as lift coefficient when designing a high-speed aircraft.
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