Effect of component deterioration on turbofan engine performance

Zhan Xue Wang, Zeng Wen Liu, Xin Nong Ye

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

The effect of component deterioration on engine performance is considerable. This influence can not be easily computed with normal engine steady performance computer program. A new mathematical method and computer program were developed to accurately compute the effect of component deterioration on engine performance. First, the mechanisms of the effect of component deterioration on engine performance were analyzed; then, statistical method was used to calculate this influence. Taking a turbofan engine as an example, the effect of component deterioration on engine performance, such as specific fuel consumption and temperature at turbine inlet was computed with this method, and compared with experimental data. The results indicate that the mathematical model in this paper can be used to compute the effect of component deterioration on engine performance.

源语言英语
页(从-至)792-796
页数5
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
22
5
出版状态已出版 - 5月 2007

指纹

探究 'Effect of component deterioration on turbofan engine performance' 的科研主题。它们共同构成独一无二的指纹。

引用此