超燃燃烧室小肋片/气动斜坡结构组合研究

Numerical study on supersonic combustor using ethylene with pylon and aero-ramp combustion

  • 摘要: 为设计出一种能有效增强掺混、提高燃烧效率的燃料喷注方案,首次将锥形肋片与气动斜坡进行结构组合研究,并对小肋片/气动斜坡不同组合方式冷、热流场进行数值模拟,分析结果发现:与传统的气动斜坡喷射相比,多肋片展向组合后方喷射能取得较为理想的掺混效果,并且不会带来较大总压损失;引入燃气发生器后,肋片的掺混增强效果得到明显提升。改善后的喷射方案能提高约9%的燃烧效率。

     

    Abstract: In order to design a fuel-injection scheme that could effectively enhance mixing and improve combustion efficiency, in this paper, the structural combination of conical pylon and aero-ramp was studies for the first time, and numerical simulation was carried out upon the cold and hot flow fields of the small pylon/aero-ramp. The experimental results show that:compared with the injection of traditional aero-ramp, the rear injection of multiple pylons in the extended composites can achieve a better mixing effect without causing a large total pressure loss. With the gas generator introduced, the mixing enhancement effect of the pylons is improved significantly. The improved injection scheme can increase the combustion efficiency by approximately 9%. The numerical results can provide certain reference for engineering practice.

     

/

返回文章
返回