摘要
研究了航空发动机部件级模型,考虑了容积惯性;采用无迭代法保证模型的实时性,并较详细地研究了初值条件较详细的研究。给出了某型发动机慢车以上状态的气体热、动力学实时模型仿真结果。
An aeroengine real - time model was constructed with the component - by - component method considering volume dynamics. The non- iterative method was adopted to ensure a good real - time model performamce. The simulated results of power ratings were presented for the aeroengine.
出处
《航空发动机》
2004年第2期35-38,58,共5页
Aeroengine
