摘要
应用时空守恒元和解元CE/SE方法,发展了求解化学反应流场的三维并行计算程序。为验证程序,对超声速冲压喷射燃烧室模型进行了计算,计算结果与实测数据以及相关文献的计算结果吻合较好,验证了本文的处理方法和程序的正确性。采用H2和O2的8组分34基元化学反应模型,对不同长深比的凹槽燃烧流动进行了数值模拟,分析了凹槽增强混合对稳定火焰的作用。计算结果表明,CE/SE方法具有模拟凹槽超声速燃烧流动的能力,数值模拟的结果有助于认识凹槽的火焰稳定机理。
A three-dimensional parallel program based on unstructured grid for reacting flows was developed using the CE/ SE method. Firstly, a seramjet eombustor model was chosen to validate the present program. The computed resuhs agree well with the experimental data. And then, the cavity combustion flows with three length-to-depth ratios were simulated under stoi- ehiometrie conditions by using 8-species, 34-elementary reaction model. The flame-holding and mixing enhancement charac- teristics of the cavities were evaluated. It demonstrates that CE/SE method is able to simulate the supersonic combustion of cavities, and the numerical studies can help understand the flame holding mechanism of the cavity.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2010年第1期34-41,共8页
Journal of Propulsion Technology