摘要
回顾了高温气体动力学与高超声速科技相关的一些重要研究进展,探讨几个具有基础性研究意义的方向：即高超声速流动模拟；高温气体热化学反应机制；高超声速流动滞止区预测；高超声速边界层转捩和激波/激波相互作用诱导的气动热问题．这些研究方向与高温气体效应和强激波密切相关,对高超声速科技关键技术的突破起着重要作用．
Some important research progresses of high temperature gas-dynamics related to hypersonic sciences and technologies are reviewed. Several fundamental research topics are discussed for future research, which include the advanced hypersonic test facilities; modeling aero-thermo-chemistry; stagnation flow region prediction; hypersonic boundary layer transition and shock waves/viscous interactions. The physical flow phenomena in such situations are thought to be closely related to real gas effects and strong shock wave interactions. It is believed that future improvements of hypersonic critical techniques depend on better understanding of those phenomena.
出处
《力学与实践》
CSCD
北大核心
2006年第5期1-7,共7页
Mechanics in Engineering
