航空学报 > 1985, Vol. 6 Issue (5): 495-497

钝体火焰稳定器冷态回流区流场的数值计算研究

曾求凡, 盛益谦, 周谦   

  1. 南京航空学院
  • 收稿日期:1984-05-20 修回日期:1900-01-01 出版日期:1985-10-25 发布日期:1985-10-25

CALCULATION OF RECIRCULATING FLOW BEHIND FLAME-HOLDERS

Zeng Qiufan, Sheng Yiqian, Zhou Qian   

  1. Nanjing Aeronautical Institute
  • Received:1984-05-20 Revised:1900-01-01 Online:1985-10-25 Published:1985-10-25

摘要:

一、计算方法 火焰稳定器是航空喷气发动机加力燃烧室的主要部件,钝体稳定器的回流区流场计算是研究加力燃烧室的重要手段,本文就二元锲形、V形和非常规截头式等三种火焰稳定器的回流区流场进行了计算研究,计算流场为二元等温定常流,紊流采用k—ε双方程模型描述。

Abstract:

Adoptability of standard k-ε turbulence model for numerical calculation of recirculating flow is discussed. Many computations of recir-culating flows behind bluff-bodies used as flame-holders in afterburner of aeroengine have been completed. Blocking-off method to treat the incline walls of the flame-holder gives good results. In isothermal recirculating flows the flame-holder wall is assumed to be isolated. Therefore, it is possible to remove the inactive zone from the calculation domain in programming to save computer time. The computation for a V-shaped flame-holder exhibits an interesting phenomenon that the recircu-lation zone extends to the cavity of the flame-holder.