Modeling and Simulation of Turbofan Engine Based on Modularized Subassembly

Article Preview

Abstract:

This paper established a nonlinear model of a turbofan engine by modularizing the components. It selected and key section parameters and to carry the numerical simulation through. The calculated results which achieved by the computer were compared with test data. It shows that the results meet the accuracy requirement. And it also provides the means to establish the engine half-physical simulation test platform.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

353-357

Citation:

Online since:

August 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Qusai Z. Al-Hamdan, Munzer S. Y. Ebaid. Modeling and Simulation of a Gas Turbine Engine for Power Generation. Transactions of the ASME. Vol. 128, APRIL (2006).

Google Scholar

[2] Liu Daxiang. Development and suggestions of aviation engine technology, China Engineering Science. 1999, VL(2): 24-9.

Google Scholar

[3] Fan Siqi. Aero engine control. Northwestern Polytechnical University Press. 2008. 6.

Google Scholar

[4] Wu Daguan. Study on the Performance of Turbofan Engine and its System, Defense Industry Press, 1986. 12.

Google Scholar

[5] Tang Zhen, Jin Jianming, Li Zhijie. Calculation method. Higher Education Press. 1992. 9.

Google Scholar

[6] Xia Fei, Huang Jinquan, Zhou Wenxiang. Research on Aeroengine Modeling and Simulation based on MATLAB/SIMULINK. Journal of Aerospace Power. 2007, 22 (12): 2134-2138.

Google Scholar