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一种分析弹性飞机总体运动稳定性及颤振特性的统一方法
引用本文:刘千刚,杨永年. 一种分析弹性飞机总体运动稳定性及颤振特性的统一方法[J]. 航空学报, 1988, 9(9): 409-417
作者姓名:刘千刚  杨永年
作者单位:西北工业大学(刘千刚),西北工业大学(杨永年)
摘    要:
 本文应用非定常气动力理论计算了刚体运动与弹性运动耦合的飞机运动方程中的非定常气动力及广义气动力导数,给出一种分析飞机总体运动稳定性及颤振特性的统一方法。

收稿时间:1987-07-11;

A UNIFIED APPROACH TO THE OVERALL BODY MOTION STABILITY AND FLUTTER CHARACTERISTICS OF ELASTIC AIRCRAFT
Liu Qiangang and Yang Yongnian. A UNIFIED APPROACH TO THE OVERALL BODY MOTION STABILITY AND FLUTTER CHARACTERISTICS OF ELASTIC AIRCRAFT[J]. Acta Aeronautica et Astronautica Sinica, 1988, 9(9): 409-417
Authors:Liu Qiangang and Yang Yongnian
Affiliation:Northwestern Polyiechnical University
Abstract:
A Green's function method for fully unsteady aerodynamics around three-dimensional bodies is outlined. This method can be used to evaluate the unsteady aerodynamic loads and derivatives of elastic aircraft. The equations of motion of an elastic aircraft are presented. And a unified method is employed to analyse the overall body motion stability and the flutter characteristics of an elastic aircraft. Numerical examples show that the results of the present method are in good agreement with the results of other methods.
Keywords:overall body motion stability   flutter   unsteady aerodynamic.
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