The analysis and computation of chemical non-equilibrium hypersonic wakes are important tasks of reentry aerodynamics. 高超音速化学非平衡尾迹流场的分析及计算是再入空气动力学的一个重要课题。
In order to grasp the hypersonic vehicle models complex dynamic characteristics, a new hypersonic vehicle model method was proposed. 摘要为了掌握高超音速飞机复杂的动态特性，提出了一种研究高超音速飞机模型的新方法。
