北京航空学院
Published:1986
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Zhu Xingjian, Wang Xueyu, Yan Qingjin, et al. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. 1986, 1(2).
DOI:
Zhu Xingjian, Wang Xueyu, Yan Qingjin, et al. CONVERGENCE OF PERFORMANCE CALCULATION OF TWIN SPOOL TURBOJET AND TURBOFAN[J]. 1986, 1(2). DOI:
本文提出了符合发动机物理模型的多变量非线性方程组的降阶处理方法
与其它各项措施相配合
可以使双轴涡喷、涡扇发动机在任何飞行状态和任何油门位置下的稳态特性计算以及在任何飞行条件下从慢车到最大状态的加速过程计算都能获得比较满意的结果。
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.
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