切向旋流对SRR补燃室内气流掺混影响  

Influence of tangential rotational jet on the mixing effect in additional chamber of solid ram rocket

作　　者：李强[1] 胡春波[1] 何洪庆[1] 蔡体敏[1] 

机构地区：[1]西北工业大学航天工程学院,陕西西安710072

出　　处：《推进技术》2003年第4期300-302,共3页Journal of Propulsion Technology

基　　金：国防重点实验室基金 (99JS60 ZS60 0 5)。

摘　　要：采用N S和k ε双方程湍流模型,离散后采用迎风格式进行数值求解,对燃气发生器喷管不同旋流工况下,管道式固体火箭冲压发动机补燃室内燃气与空气掺混进行了数值研究。比较分析了不同旋流角对补燃室中掺混效果的影响。计算表明:在0°～20°计算范围内,随着旋流角度的增加,补燃室中高温燃气和冷空气的掺混更充分。Using the N-S and k-Ε turbulence model and upwind scheme, numerical studies on the mixing effects of burning gas and air in the additional chamber of solid ramjet motor were carried out under different rotational angles. After comparison, the influences of rotational angles on mixing effect were analyzed. The numerical results show that the mixing effects increase as rotational angle increases when it is smaller than 20°C.

关 键 词：冲压火箭发动机 加力燃烧室 混合 旋流角 

分 类 号：V236[航空宇航科学与技术—航空宇航推进理论与工程]