为了验证牛顿流理论的效度,在高超声速高温气体效应下设计验证模型,对比牛顿流理论解析解和数值模拟结果,证明牛顿流理论在高温气体效应下仍然具有相当高的效度。研究表明完全气体模式下的牛顿理论仍然可以移植到高温气体情形下,在高温气体效应下为飞行器设计提供前期的概念指导。 In order to verify the validity of the Newtonian theory, the verification model was designed under the effect of hypersonic high temperature gas. Compared with the Newtonian theory and numerical simulation results, it is proved that the Newtonian theory still has a very high validity under high temperature gas effect. The results show that the Newton theory in complete gas mode can still be transplanted to high temperature gas and provide early conceptual guidance for aircraft design under the effect of high temperature gas.