[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

弹箭与制导学报 >

2021 , Vol. 41 >Issue 3: 15 - 20

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.03.004

导流片结构参数对三通道进气TVC性能影响

  • 姚婷 ,
  • 刘景源
展开
  • 南昌航空大学飞行器工程学院,南昌 330063

姚婷(1995—),女,江苏南京人,硕士研究生,研究方向:航空宇航推进理论与工程。

收稿日期: 2019-07-12

  网络出版日期: 2025-02-20

基金资助

国家自然科学基金(11102079)

国家自然科学基金(11562012)

收起

Effects of Flow Guide Vanes Structure Parameters on Characteristics of A Three-duct TVC

  • YAO Ting ,
  • LIU Jingyuan
Expand
  • School of Aircraft Engineering, Nanchang Hangkong University, Nanchang 330063, China

Received date: 2019-07-12

  Online published: 2025-02-20

Fold

摘要

对不同导流片结构参数下三通道进气驻涡燃烧室的流场分布、燃烧效率及总压损失系数进行数值模拟。结果显示,凹腔内形成理想双涡结构,增强了凹腔与主流的热质掺混,稳定凹腔点火源,大幅度提升燃烧效率。导流片结构参数a/E对燃烧效率、总压损失系数的影响最大,b/H、c/L对燃烧效率几乎没有影响,c/L对总压损失系数影响较大;当a/E=0.5,b/H=0.5及c/L=0.5时,燃烧室性能最佳,燃烧效率99.669 8%,总压损失系数3.126 8%。

关键词： 驻涡燃烧室; 导流片; 燃烧效率; 总压损失系数; 数值模拟

本文引用格式

姚婷 , 刘景源 . 导流片结构参数对三通道进气TVC性能影响[J]. 弹箭与制导学报, 2021 , 41(3) : 15 -20 . DOI: 10.15892/j.cnki.djzdxb.2021.03.004

Abstract

The influence of different structural parameters of a three-duct trapped vortex combustor(TVC) with flow guide vanes on flow fields, combustion efficiency and total pressure loss coefficient are numerically studied. The results show that the ideal dual vortices can be formed in the cavity, which enhance the stability of flame and the mixing of gas, combustion efficiency. The structure parameter a/E influences the performance of the TVC significantly, while the changes of b/H and c/L have little effect on the combustion efficiency, but c/L has some effects on the total pressure loss coefficient. When a/E=0.5, b/H=0.5, c/L=0.5, the best performance of the TVC is achieved with the combustion efficiency 99.669 8%, the total pressure loss coefficient 3.126 8%.

Key words： trapped vortex combustor; flow guide vanes; combustion efficiency; total pressure loss coefficient; numerical simulation

[an error occurred while processing this directive]

参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序
[1]
DENG Y B, SU F M. Low emissions trapped vortex combustor[J]. Aircraft Engineering and Aerospace Technology, 2016, 88(1): 33-41.

[2]
KUMAR P K E, MISHRA D P. Flame stability characteristics of two-dimensional trapped vortex combustor[J]. Combustion Science and Technology, 2016, 188(8): 1283-1302.

[3]
ZHANG R C, FAN W J. Experimental study of entrainment phenomenon in a trapped vortex combustor[J]. Chinese Journal of Aeronautics, 2013, 26(1): 63-73.

[4]
AGARWAL K K, RAVIKRISHNA R V. Experimental and numerical studies in a compact trapped vortex combustor: stability assessment and augmentation[J]. Combustion Science and Technology, 2013, 183(12): 1308-1327.

[5]
曾卓雄, 郭帅帅, 王浩渊. 不同进口条件对微小尺寸驻涡燃烧室性能的影响[J]. 热科学与技术, 2018, 17(6):431-436.

[6]
韩吉昂, 李晓东, 钟兢军. 环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比[J]. 航空动力学报, 2015, 30(2):331-340.

[7]
王志凯, 曾卓雄, 徐义华, 等. 导流片结构参数对先进旋涡燃烧室性能影响研究[J]. 推进技术, 2015, 36(3):405-412.

[8]
俞骏, 刘景源. 带导流片的三维环形驻涡燃烧室的数值分析[J]. 弹箭与制导学报, 2018, 38(1):55-60.

[9]
俞骏, 周韦韦, 刘景源. 一种三通道进气先进旋涡燃烧室性能数值分析[J]. 弹箭与制导学报, 2017, 37(4):92-97.

[10]
AGARWAL K K, RAVIKRISHNA R V. Experimental and numerical studies in a compact trapped vortex combustor: stability assessment and augmentation[J]. Combustion Science and Technology, 2011, 183(12): 1308-1327.

Options
文章导航

/

〈 〉

[an error occurred while processing this directive]