(北京航空材料研究院 2室， 北京 100095)
摘 要: 利用快速圖像采集技術(shù)研究了Al-TiO2C體系燃燒過(guò)程，基于燃燒理論建立了Al-TiO2C三元SHS燃燒過(guò)程數(shù)學(xué)模型，并進(jìn)行了數(shù)值模擬工作，模擬結(jié)果與實(shí)驗(yàn)結(jié)果得到了較好的吻合，由此進(jìn)一步分析了Al-TiO2C體系燃燒過(guò)程的特征及其轉(zhuǎn)變規(guī)律。
關(guān)鍵字: SHS； 燃燒過(guò)程； 計(jì)算機(jī)模擬
simulation in Al-TiO2C system
（No2 Lab， Beijing Institute of Aeronautical Materials，
Beijing 100095, P.R.China）
Abstract: The combustion process in Al-TiO2C system was studied by means of the rapid image sampling technique. Based on the combustion theories a mathematics model of the SHS combustion process in Al-TiO2C system has been built and numerical simulation has been done. The calculation results are in good agreement with the experimental results. Then the characteristic and the changing law of the combustion process in Al-TiO2C system have been analyzed.
Key words: SHS； combustion process； computer simulation
