On the Calculation of Wall and Coolant Temperatures of Regeneratively Cooled Rocket Engines.

被引：0
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作者：
Reinkenhof, J.
机构：
来源：
Deutsche Luft- und Raumfahrt, Forschungsbericht | 1972年 / 72-29期
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中图分类号：
V4 [航天（宇宙航行）]; V238 [];
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摘要：
A differential equation for the temperature of the coolant flow is derived. The temperature distribution in the wall is given as a polynomial function. The temperature dependence of the heat conductivity of the wall material is taken into account. The calculation method is applied to a LO//2/LH//2- high-pressure rocket engine.
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