高马赫数飞行器壁面质量引射流量分配多目标优化

邹昊,胡国暾,邱云龙,石伟,陈伟芳

Multi-objective optimization of wall mass injection flow ratedistribution for hypersonic vehicle

Hao ZOU,Guotun HU,Yunlong QIU,Wei SHI,Weifang CHEN

图 14 不同引射方案头部壁面附近(Y = 0.04 m, Z = 0 m)沿飞行器的轴向温度分布

Fig.14 Axial temperature distribution along aircraft near head wall (Y = 0.04 m, Z = 0 m) for different injection schemes