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螺旋颤振分析
引用本文:金一忱.螺旋颤振分析[J].航空学报,1993,14(4):210-213.
作者姓名:金一忱
作者单位:西安市72~303信箱 西安
摘    要: 对于装有螺旋桨发动机、涡轮螺桨发动机的飞机,存在着螺桨与发动机组合的螺旋颤振稳定性问题。本文介绍~种实用的分析方法,取沉浮、侧向平动、俯仰、偏航4个自由度,以准定常方法计算出螺旋桨气动力,并计入陀螺力矩,形成系统状态方程,然后提取特征值,以确定系统的稳定性。算例中还对影响稳定性的若干参数进行了分析。

关 键 词:气功弹性  螺旋颤振  稳定性  螺旋桨  

WHIRL FLUTTER ANALYSIS
Jin Yi-chen.WHIRL FLUTTER ANALYSIS[J].Acta Aeronautica et Astronautica Sinica,1993,14(4):210-213.
Authors:Jin Yi-chen
Institution:BOX 72-303 of Xi'an, Xi'an 710089
Abstract:The whirl flutter stablility of the engine-propeller installation is related to the aircraft with propeller, turboprop, or propfan engines. In this paper a practical method is presented to analyse the problem. In the analysis four degrees of freedom, namely vertical and horizontal displacements, pitch and yaw, are considered. Quasi-steady propeller aerodynamics and gyroscopic moment are added to the dynamic equation. From the system slate equation obtained . eigenvalues, eigenvecters are abstracted to predict and analyse the system's stability. Based on an example data, the effects of several parameters on the stability are also studied.
Keywords:aeroelasticity  whirl flutter  stability  propeller
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