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一种波瓣混合器超级燃烧室的掺混特性
引用本文:程晓军,范育新,蔡迪,王家骅.一种波瓣混合器超级燃烧室的掺混特性[J].航空动力学报,2014,29(7):1606-1614.
作者姓名:程晓军  范育新  蔡迪  王家骅
作者单位:南京航空航天大学 能源与动力学院, 南京 210016;南京航空航天大学 能源与动力学院, 南京 210016;南京航空航天大学 能源与动力学院, 南京 210016;南京航空航天大学 能源与动力学院, 南京 210016
基金项目:江苏省普通高校研究生科研创新计划(CXZZ12_0167)
摘    要:为了使涡轮基组合循环发动机超级燃烧室的涡扇涵道和冲压涵道两股气流具有高效低阻的掺混特性,设计了一种结构简单的方形波瓣混合器.用数值模拟方法对该方形波瓣混合器与常规混合器进行了比较分析,结果表明方形波瓣混合器具有与菊花型波瓣混合器相似的流向涡高效低阻掺混特性.进行混合器结构参数变化对掺混特性的影响研究发现扩张角对方形波瓣混合器的热混合效率的影响起主要作用,而出口高度的影响不大;当方形波瓣混合器的波长比为1.0时,方形波瓣混合器具有高效低阻的掺混特性.

关 键 词:涡扇冲压组合发动机  超级燃烧室  波瓣混合器  流向涡  热混合效率  总压恢复系数
收稿时间:2013/4/17 0:00:00

Mixing characteristics of hyperburner with a lobed mixer
CHENG Xiao-jun,FAN Yu-xin,CAI Di and WANG Jia-hua.Mixing characteristics of hyperburner with a lobed mixer[J].Journal of Aerospace Power,2014,29(7):1606-1614.
Authors:CHENG Xiao-jun  FAN Yu-xin  CAI Di and WANG Jia-hua
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:A simple structure square lobed mixer with high mixing efficiency and low resistance was designed to turbofan by pass flow with ram bypass flow thoroughly in turbine based combined cycle engine hyperburner. Numerical simulation of square lobed mixer and comparative analysis with conventional mixer were made; the results indicate that square lobed mixer with high mixing efficiency and low resistance of the streamwise vortices of daisy lobed mixer. Numerical simulation results of various mixer structure parameters' influence on mixing characteristics show that expansion angle dominates the thermal mixing efficiency, and the export height of the mixer has little effect on it. The square lobed mixer has the characteristics of high mixing efficiency and low resistance when the wavelength ratio is 1.0.
Keywords:turbine based combined cycle  hyperburner  lobed mixer  streamwise vortex  thermal mixing efficiency  total pressure recovery coefficient
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