| 微型涡轮喷气发动机蒸发管式燃烧室数值模拟 |
| |
| 引用本文： | 郭渊,蒋雪辉,郑严. 微型涡轮喷气发动机蒸发管式燃烧室数值模拟[J]. 战术导弹技术, 2011, 0(1): 109-113 |
| |
| 作者姓名： | 郭渊 蒋雪辉 郑严 |
| |
| 作者单位： | 中国航天科工集团第三研究院; |
| |
| 摘 要： | 对推力为40 daN的微型涡轮喷气发动机蒸发管式燃烧室进行了设计工况下的数值模拟,得到了燃烧室内流场分布、温度场分布以及燃烧室性能参数.通过数值模拟得到了微型发动机蒸发管式燃烧室的一些特性规律,为燃烧室的设计提供参考依据.
|
| 关 键 词： | 微型涡轮喷气发动机 蒸发管式燃烧室 数值模拟 |
Numerical Simulation for the Combustor with Vaporizing Tube of Micro Turbojet Engine |
| |
| Guo Yuan,Jiang Xuehui,Zheng Yan. Numerical Simulation for the Combustor with Vaporizing Tube of Micro Turbojet Engine[J]. Tactical Missile Technology, 2011, 0(1): 109-113 |
| |
| Authors: | Guo Yuan Jiang Xuehui Zheng Yan |
| |
| Affiliation: | Guo Yuan,Jiang Xuehui,Zheng Yan(The Third Research Academy,CASIC,Beijing 100074,China) |
| |
| Abstract: | The design condition performances are simulated for the combustor with vaporizing tube of 40daN micro turbojet engine.The combustor flow field,temperature field and the performance parameters of the combustor are received.Then,the features of the combustor with vaporizing tube of micro turbojet engine are acquired by simulation,and reference basis for the design of the combustor can be supplied. |
| |
| Keywords: | micro turbojet engine combustor with vaporizing tube numerical calculation |
| 本文献已被 CNKI 维普 等数据库收录！ |
|
