利用高精度差分格式求解了可压缩n - S方程球头热流问题。
A high order accurate upwind compact difference scheme for N-S equations is developed.
在航天器地面热试验中，空间热流的模拟是一个非常复杂而重要的问题。
The simulation of Space heat flux is a very complicated and important problem in ground thermal testing of spacecraft.
通过系统地分析窖温、风温以及热流，发现了沟窖几个重要的热工问题。
Some thermotechnical problems are revealed through systematic analysis of temperature, air flow as well as heat flux in cellar.
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