摘要
对某型发动机燃烧室在高空、低速条件下的燃烧稳定性进行了分析,并对燃烧效率进行了计算。结果表明:20km高空,0 7M飞行条件下,燃烧室能实现稳定燃烧,燃烧效率高。
The engine combustion stability is analyzed and the combustion efficiency is calculated under the condition of high altitude and low velocity. The result indicates that when H = 20km, M = 0.7, the combustion in the chamber is smooth and the combustion efficiency is high.
出处
《空军工程大学学报（自然科学版）》
CSCD
2004年第2期6-8,共3页
Journal of Air Force Engineering University(Natural Science Edition)
基金
863计划项目(2002AA753012)
关键词
燃烧稳定性
燃烧效率
航空发动机
combustion stability
combustion efficiency
aircraft engine
