Numerical analysis of exhaust jet secondary combustion in hypersonic flow field
- 点击次数：
- 所属单位：航空学院
- 发表刊物：MODERN PHYSICS LETTERS B
- 关键字：Exhaust jet secondary combustion amplification factor hypersonic numerical analysis
- 摘要：The interaction effect between jet and control surface in supersonic and hypersonic flow is one of the key problems for advanced flight control system. The flow properties of exhaust jet secondary combustion in a hypersonic compression ramp flow field were studied numerically by solving the Navier Stokes equations with multi-species and combustion reaction effects. The analysis was focused on the flow field structure and the force amplification factor under different jet conditions. Numerical results show that a series of different secondary combustion makes the flow field structure change regularly, and the temperature increases rapidly near the jet exit.
- ISSN号：0217-9849
- 是否译文：否
- 发表时间：2018-05-10
- 合写作者：Yang, Tian-Peng,Zhao, Fa-Ming,Fan, Xiao-Feng,Wang, Yu-Han
- 通讯作者：王江峰
- 发表时间：2018-05-10
