烧蚀防护罩;
According to the thermal shielding model of solid rocket motor, an approach of ablation heat shield design of end-burning grain with embedded wire was put forward in this paper.
根据固体火箭发动机绝热防护模型,提出了一种嵌金属丝端燃装药绝热层设计方法。
The transpiration cooling control of the thermal protective shield with surface ablation appears as a nonlinear control system of distributed parameters on a variable domain.
热防护层表面有烧蚀的发汗冷却控制是一个活动边界域上分布参数的非线性控制系统。
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