Thermal Protection Modeling of Hypersonic Flying Apparatus by A. S. Yakimov

Author:A. S. Yakimov
Language: eng
Format: epub
Publisher: Springer International Publishing, Cham

(2.4.2)

For the sake of simplicity, we assume that:(1)the Reynolds number in the incident high-entropy airflow is sufficiently high (, and a boundary layer was formed in the vicinity of the body surface;

(2)the thermal protective material is a two-temperature medium, i.e., the liquid–vapor and condensed phases have different temperatures;

(3)the mass flow rate at a normal to the plate in flow is significantly greater than that the mass flow rate along this plate (Fig. 2.12, );

(4)the permeable medium I–II (Fig. 2.12) consists of three components: inert frame, water, and superheated vapor;

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