Abstract

The paper presents the methods and results of the calculation of flow around a return vehicle accounting for the physical and chemical processes in the flow field during aerodynamic braking in the Earth’s atmosphere. The models of chemical processes proceeding in the shock layer at the vehicle surface and corresponding to various initial and boundary conditions are studied.

中文翻译：

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大气回程飞行器轨迹上激波层理化过程的数值研究

摘要

本文介绍了计算返航车辆周围流量的方法和结果，说明了大气中空气动力制动过程中流场中的物理和化学过程。研究了在车辆表面的冲击层中进行的化学过程模型，该模型与各种初始条件和边界条件相对应。