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Paper 219

Estimation of the Critical Flutter Load of a Double L-shaped Beam subjected to Follower Forces (In-Plane Vibration)

doi:10.4203/ccp.106.219

I. Takahashi, "Estimation of the Critical Flutter Load of a Double L-shaped Beam subjected to Follower Forces (In-Plane Vibration)", in , (Editors), "Proceedings of the Twelfth International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 219, 2014. doi:10.4203/ccp.106.219

Keywords: Response surface approximation, design of experiments, double L-shaped beam, natural frequency, critical flutter load, follower force, in-plane vibration..

Summary

With increasing size and complexity of machines and vessels, the inverse problems of continuous bodies are becoming important. In this paper the possibility of using a response surface methodology, which consists of a design of experiments, for estimating the critical flutter load of the double L-shaped beam is studied. An analysis is presented for the in-plane vibration and stability of a non-uniform doublebeam subjected to tangential follower forces distributed over the center line by use of the transfer matrix approach.

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Front Page Browse CCP CSETS CTR IJRT Other Authors Search Purchase Guide FAQ Contact us	Civil-Comp Proceedings ISSN 1759-3433 CCP: 106 PROCEEDINGS OF THE TWELFTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by: Paper 219 Estimation of the Critical Flutter Load of a Double L-shaped Beam subjected to Follower Forces (In-Plane Vibration) I. Takahashi Department of Mechanical Engineering, Kanagawa Institute of Technology, Japan doi:10.4203/ccp.106.219 purchase the full-text of this paper Full Bibliographic Reference for this paper I. Takahashi, "Estimation of the Critical Flutter Load of a Double L-shaped Beam subjected to Follower Forces (In-Plane Vibration)", in , (Editors), "Proceedings of the Twelfth International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 219, 2014. doi:10.4203/ccp.106.219 Keywords: Response surface approximation, design of experiments, double L-shaped beam, natural frequency, critical flutter load, follower force, in-plane vibration.. Summary With increasing size and complexity of machines and vessels, the inverse problems of continuous bodies are becoming important. In this paper the possibility of using a response surface methodology, which consists of a design of experiments, for estimating the critical flutter load of the double L-shaped beam is studied. An analysis is presented for the in-plane vibration and stability of a non-uniform doublebeam subjected to tangential follower forces distributed over the center line by use of the transfer matrix approach. purchase the full-text of this paper (price £20) go to the previous paper go to the next paper return to the table of contents return to the book description purchase this book (price £65 +P&P)
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