节点文献

脉冲爆轰发动机第一和第二次循环的数值模拟

Numerical simulation of 1st and 2nd cycles of pulse detonation engine

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 于陆军范宝春归明月董刚

【Author】 YU Lu-jun,FAN Bao-chun,GUI Ming-yue,Dong Gang(Laboratory of Transient Physics,Nanjing University of Science and Technology,Nanjing Jiangsu 210094,China)

【机构】 南京理工大学瞬态物理实验室

【摘要】 对脉冲爆轰发动机两次循环工作过程进行轴对称数值模拟,考虑了包含19个基元反应和9种组份的H2-O2-N2详细化学反应动力学机理,通过改进的ISAT方法(动态自适应建表)减少反应化学的计算时间。数值结果显示了脉冲爆轰发动机充气,起爆,卸压和再充气的循环工作过程。根据数值计算结果,详细地讨论了两次循环管内、外流场的结构间的差异。两次循环中管内、外流场结构的差异又导致二者推力和冲量的不同。

【Abstract】 By solving axisymmetric Navier-Stokes equations in conjunction with the chemistry,numerical simulation of two cycle of pulse detonation engine was performed,and a detailed chemical mechanism of H2-O2-N2 system,which included 19 element reactions and 9 species,was involved.An in situ adaptive tabulation(ISAT) method was improved to enhance the computational performance of combustion chemistry.The calculated results showed the process of fueling,initiation,blowing down and refueling.Based on the numerical results,the difference of dynamics mechanism of external flow field between 1st cycle and 2nd cycle was elucidated systematically.Thrust and impulse during two cycles varied with the difference of the flow pattern in the internal and external flow fields.

【基金】 国家自然科学基金项目(10472047,50336030);北京理工大学爆炸科学与技术重点实验室开放基金(KFJJ06-3)
  • 【文献出处】 空气动力学学报 ,Acta Aerodynamica Sinica , 编辑部邮箱 ,2009年04期
  • 【分类号】O381
  • 【被引频次】3
  • 【下载频次】149
节点文献中: 

本文链接的文献网络图示:

本文的引文网络