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压气机特性线应用于发动机线性建模的新算法
引用本文:刘建勋,苗学问.压气机特性线应用于发动机线性建模的新算法[J].航空计算技术,2001,31(3):12-15,18.
作者姓名:刘建勋  苗学问
作者单位:空军工程大学工程学院,陕西西安,710038
摘    要:基于某型航空发动机的基本方程 ,建立了其线性数学模型。着重解决了两个问题 :提出一种改进的分段光滑插值 ,代替通常的插值方法来获得所需参数及偏微分量 ;给出了从压气机换算参数的偏微分到物理参数的偏微分的转换公式。最后基于MATLAB进行了动态特性的数字仿真

关 键 词:混排涡扇发动机  线性数学模型  光滑  插值
修稿时间:2001年4月30日

New Methods for Application of Compressor Characteristic Curve in Linear Mathematic Model Study of Aero-Engine
LIU Jian-xun,MIAO Xue-wen.New Methods for Application of Compressor Characteristic Curve in Linear Mathematic Model Study of Aero-Engine[J].Aeronautical Computer Technique,2001,31(3):12-15,18.
Authors:LIU Jian-xun  MIAO Xue-wen
Abstract:Based on the basic equation of an certain type of aero-engine, a linear mathematic model is established in this paper. Two problems are solved mainly. Firstly, an improved piecewise smooth interpolation, which will replace the usual interpolation method, is presented to acquire needed parameters and partial differential values. Then, conversion formulae are given to acquire values of physical parameter partial differential from calculating parameter partial differential. Finally, computer simulation of dynamic characteristic under MATLAB environment is performed.
Keywords:mixed exhaust turbofan  linear mathematic model  smooth  interpolation  
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