Dynamic Properties and Fatigue Failure of Aircraft Component

Abstract

The basic purpose of given article is consideration of the problems connected with application of a method of concentrated weights in the tasks of mechanical systems dynamics at non-classic internal and external constraints. The method of the concentrated weights is convenient means of the analysis of dynamic properties of elastic mechanical systems. It has relative simplicity of definition of the parameters of equivalent discrete system, the clearness of computing algorithms and provides comprehensible accuracy of definition of the lowest natural frequencies. Doubtless advantage of a method is convenience of modeling of non-classic constraints of fastening and internal constraints between elements of complex systems. Such problems arise at the decision of practice tasks of the analysis of dynamics of real systems. The method is used for the analysis of vibra-tions of a beam with variable parameters at presence of elastic supporting of the beam and the attached additional concentrated weight. A result of dynamic analysis has a good correlation with the fatigue damages observed at fatigue test of a beam.

On the Dynamic Response Prediction at the Full-Scale Test of Aircraft Component

“…This is especially important for adequate dynamic properties when planning separate component tests of the structural system [26]. In presented article, analysis is focused to comparison different kinds of boundary conditions for the same object.…”

“…In presented article, analysis is focused to comparison different kinds of boundary conditions for the same object. Problem of validation of dynamic simulation is considered in the [26].…”