Flоw аnd соmbustiоn сhаrасtеristiсs оf trарреd vоrtех саvity соmbinеd with rаdiаl flаmеhоldеr

被引:0
作者
Kang, Yudong [1 ]
Zhong, Shilin [1 ,2 ]
Peng, Weikang [1 ]
Zhai, Yunchao [1 ]
Deng, Yuanhao [1 ]
机构
[1] Sichuan Gas Turbine Establishment, Aero Engine Corporation of China, Chengdu
[2] Institute for Aero Engine, Tsinghua University, Beijing
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2025年 / 40卷 / 01期
关键词
afterburner; combustion characteristics; flow characteristics; radial flameholder angle; trapped vortex cavity flameholder;
D O I
10.13224/j.cnki.jasp.20230128
中图分类号
学科分类号
摘要
In order to improve the comprehensive combustion performance of trapped vortex cavity afterburner and better understand the effect of radial flameholder installation angle on flow and combustion characteristics, numerical and experimental investigation were employed at 5°, 8°, 10°, 15° under different excess air coefficients. The investigations were performed under the bypass temperature 600 K, the core temperature 1 000 K, the core pressure 180 kPa, the bypass ration 0.17, and excess air coefficient 1.27—2. Through investigation, the flow filed, exit temperature, total pressure recovery coefficient, wall temperature of trapped vortex cavity (TVC) and radial flameholder were obtained. The results showed that when the angle was 5°,the total pressure recovery coefficient was 0.002—0.006 lower, the exit temperature was 20—40 K higher, the TVC wall temperature was 63—82 K lower, the radial flameholder wall temperature was 60—70 K higher than that at the angle of 10°. © 2025 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
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