Analysis of the aerodynamic performance of a hypersonic gliding missile with a deflected warhead
Zhao-Kang Zhang,
Shu-Sheng Chen,
Yuan-Zhe Dong
et al.
Abstract:In this study, we propose a scheme to control the deflection of the warhead based on the configuration of the hypersonic glide body (HGB) to solve the problems posed by its large control surface load and severe aerodynamic heat under hypersonic flight conditions. We conducted numerical simulations on the configurations of deflection of the warhead of an HGB analog under different flight modes as well as varying angles and directions of deflection. The results showed that once the warhead had been deflected, th… Show more
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