摘要
为研究二次燃烧对底排尾部流场的影响,建立了底排装置尾部流场的化学非平衡流数学物理模型。其中二次燃烧模型采用10组分25步反应的H2-CO燃烧模型,运用统一算法的思路编程求解二维轴对称方程组。数值模拟结果与实验结果较吻合。在此基础上,对尾部流场以及燃烧特性进行了数值预测,结果表明:二次燃烧所释放的热能远大于排气本身的热能,对增压减阻的贡献可达78%。二次燃烧改变了尾部的温度分布规律,使温度峰值分布在两个回流区内。排气沿着两回流区间的狭缝流入剪切层发生燃烧。一部分混气回流入底部附近,其中氧气不充足,存在大量CO和少量H2未直接反应。一部分混气沿着剪切层流入下游以及主回流区内,氧含量逐渐增多,H2和CO被反应殆尽。结果可为进一步研究底排增压减阻提供参考。
In order to investigate the influence of secondary combustion for base flow field, a mathe matical and physical model about base flow with chemical non-equilibrium for base bleed equipment is conducted. H2-CO combustion model which consists 10 components and 25 reactions is used for sec ondary combustion. Two-dimensional axisymmetric equations are solved using a set of uniform nu- merical process methods. Simulation results agree with experiment data well. based on this, base flow field and combustion characteristics are numerically predicted. The results show that heat energy released from secondary combustion is far more than heat energy from bleed gases. Secondary corn bustion has a huge contribution to increase base pressure. It changes the temperature distribution of base region. Bleed gases flow into the shear layer, then combustion occurs. Some mixed gases which flow into the bottom region burn incomplete, because the oxygen is not sufficient near the bottom. Some mixed gases which flow into the downstream and main reeirculation zone burn complete, be cause the oxygen is sufficient. The results can be used as reference for further improvement of the base bleed.
出处
《爆炸与冲击》
EI
CAS
CSCD
北大核心
2015年第1期94-100,共7页
Explosion and Shock Waves
基金
国家自然科学基金项目(51176076)
关键词
流体力学
二次燃烧
化学非平衡流
底部排气
尾部流场
fluid mechanics
secondary combustion
chemical non-equilibrium flow
base bleed
base flow field