中国空间科学技术
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宋裕阳
发布日期:
Song Yuyang (Beijing Institute of Technology)
Online:
摘要: 本文介绍四层壁固体火箭发动机不稳定导热的计算方法,导出壳体温度分布规律和各层壁温的计算公式。
关键词: 导热性, 固体火箭发动机
Abstract: This paper presents a calculation of unsteady heat conduction in fourlayered slabs of solid rocket engine, deduces a regularity of the temperature distribution in chamber and the eguation of temperature calculation in every layer.
宋裕阳. 四层壁的不稳定导热[J]. 中国空间科学技术.
Song Yuyang (Beijing Institute of Technology). UNSTEADY HEAT CONDUCTN IN FOUR-LAYERED SLABS[J]. Chinese Space Science and Technology.
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链接本文: https://journal26.magtechjournal.com/kjkxjs/CN/
https://journal26.magtechjournal.com/kjkxjs/CN/Y1987/V7/I06/59