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A METHOD FOR SOLVING NON-LINEAR THERMAL PROBLEMS IN RE-ENTRY OF SPACE VEHICLES

机译:一种解决空间飞行器重新进入非线性热问题的方法

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摘要

The paper is divided into three parts In Part I a body of whatever shape is considered, of volume V, bounded by one or more surfaces 5, and with thermal coef¬ficients K and c (.conductivity and specific heat, respecti very) It is assumed - for the moment being - the geometry of the body and the coefficients c and K not to change with time The body, initially at known temperature, is assumed to be heated by a distribution of heat sources of any wanation with space and time.

著录项

  • 作者

    Luigi Broglio;

  • 作者单位
  • 年度 1961
  • 页码 1-23
  • 总页数 23
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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