With the above method, flows in transitional region around cylinder, sphere double cone and Apollo capsule are simulated. The aerodynamic and flow characteristics are analyzed.

• 最后,采用本文发展的方法,对绕圆柱、球双锥和Apollo飞船的过渡区域流动进行了数值模拟,并对其气动特性、流场特征和流动现象进行了分析。