摘要
根据低转速下的发动机部件特性的半经验数据，建立了一种通用的发动机起动计算模型，并对发动机起动控制规律进行了研究。最后以某发动机为例，详细分析了发动机的起动过程。
A generalized aeroengine startup model was developed in terms of some
semi emperical data of aeroengine conponents at low rotating speeds.The corresponding startup
control was also studied.Based on this model,a whole starting procedure of an aeroengine was
well described
出处
《推进技术》
EI
CAS
CSCD
北大核心
1999年第2期21-24,共4页
Journal of Propulsion Technology
