CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN

Zhu Xingjian; Wang Xueyu; Yan Qingjin; Zhang Xueliang

Volume 1 Issue 2

Oct. 1986

Turn off MathJax

Article Contents

Article Navigation > Journal of Aerospace Power > 1986 > 1(2): 107-110,182

Zhu Xingjian, Wang Xueyu, Yan Qingjin, Zhang Xueliang. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. Journal of Aerospace Power, 1986, 1(2): 107-110,182.

Citation:

Zhu Xingjian, Wang Xueyu, Yan Qingjin, Zhang Xueliang. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. Journal of Aerospace Power, 1986, 1(2): 107-110,182.

Zhu Xingjian, Wang Xueyu, Yan Qingjin, Zhang Xueliang. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. Journal of Aerospace Power, 1986, 1(2): 107-110,182.

Citation:

Zhu Xingjian, Wang Xueyu, Yan Qingjin, Zhang Xueliang. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. Journal of Aerospace Power, 1986, 1(2): 107-110,182.

PDF( 449 KB)

CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN

Beijing Institute of Aeronautics and Astronautics

Received Date: 1986-02-01
Publish Date: 1986-10-28

Abstract

Abstract

The calculation of steady-state performance for twin spool turbojet and tur-bofan can be performed by formulating a multi-variable nonlinear equation set with parameters.