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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 76
PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON ENGINEERING COMPUTATIONAL TECHNOLOGY Edited by: B.H.V. Topping and Z. Bittnar
Paper 80
Neural Identification for Critical Flutter Load of a Cracked Shaft Simultaneously Subjected to a Follower Force with an Axial Force I. Takahashi
Department of Mechanical Engineering, Kanagawa Institute of Technology, Japan I. Takahashi, "Neural Identification for Critical Flutter Load of a Cracked Shaft Simultaneously Subjected to a Follower Force with an Axial Force", in B.H.V. Topping, Z. Bittnar, (Editors), "Proceedings of the Third International Conference on Engineering Computational Technology", Civil-Comp Press, Stirlingshire, UK, Paper 80, 2002. doi:10.4203/ccp.76.80
Keywords: neural network, natural frequency, shaft, flutter load, cracks, axial force.
Summary
Light weight structure have been extensively used in many industrial fields such as in
mechanical, aerospace and rocket engineering, and therefore vibration and stability
problems of shafts have become of increasing importance. Especially, the majority of
the structural parts of machines are operated in the range of limited fatigue strength,
which occures the cracks in overstressed zone. The analysis of the dynamic
characteristics of cracked structural elements is an important problem in technology.
In particular, the inverse problems of cracked continuous bodies are becoming
important in design practice.
The artificial neural network is now one of the most rapidly expanding area of research across many disciplines [1,2]. In mathematical fields the neural network is an effective mapping tool-mapping an input vector to an output vector. On the other hand, the identification technique for support conditions of continuous bodies is becoming important, with the increasing size and complexity of machines and vessels. Yasuda and Goto [3] and Kamiya, et al. [4] proposed the experimental identification technique for boundary conditions of the beam. Saito, et al. [5] and Yasuda, et al. [6] presented the identification of non-linear support systems by using transient response. Takahashi [7,8] proposed the identification method for the axial force (or critical force) and boundary conditions of a beam using the neural networks. In this paper the possibility of using a Multilayer Perceptron Network trained with the Backpropagation Algorithm for identifying the critical flutter load and support conditions (or shape parameters) of the cracked shaft is studied. The natural frequecies which are the most fundamental and simplest in the modal parameters are adopted here to estimate the flutter load and support conditions (or shape parameters). The basic idea is to train a neural network with simulated patterns of the relative changes of natural frequencies and corresponding support condition (or shape parameters) and critical flutter load of shafts in order to recognize the behaviour of the shaft. Subjecting this neural network to un-learning natural frequencies should imply information about the support condition (or shape parameters) and critical flutter load of shafts. The training data are obtaining by the values using the transfer matrix method. By a trial-and-error approach, with a view of simplify the network structure and speed up the convergence of the algorithm, we defined the network of three layers. The neural networks were trained with numerical values of the relative changes of the lowest four frequency parameters of shafts. From the results of the numerical examples we can draw the following conclusions. The support condition (or shape parameters) and critical flutter load of shafts can be predicted by the change in frequency parameters. References
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