Investigation on supersonic combustion of fuel-rich hot gas as reacting jets in ramjet/scramjet combustor

被引：0
|
作者：
Situ, M. [1 ]
Wang, C. [1 ]
Lu, H.P. [1 ]
机构：
[1] 31st Res. Inst., Beijing 100074, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2001年 / 22卷 / 03期
关键词：
Combustion - Kerosene - Supersonic flow - Test facilities - Testing;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The experiments were set on the ground connected pipe test station with air mass rate of 1.2 kg/s. The characteristics and performances of supersonic combustion of fuel-rich hot gas as reacting jets injected into the combustor with dual-cavity configuration were investigated by means of pressure measurement and photo. The results show that the ignition of supersonic combustion is reliable and the combustion flame is stable. Furthermore, the efficiency of supersonic combustion is more than 0.80. The present new scheme of supersonic combustion is an attractive candidate for ramjet/scramjet.
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页码：237 / 240
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