Differential transformation method for free vibration analysis of an axially loaded overhung rotor

Author:

Bensabri Omar1ORCID,Hamza-Cherif S. M.2,Mankour Abdeljelil1

Affiliation:

1. Department of Research in Space Mechanics, Satellite Development Center (CDS), BP4065, Ibn Roched, Oran 31100, Algeria

2. MECACOMP Laboratory, Department of Mechanical Engineering, Faculty of Technology, University of Tlemcen, Tlemcen, Algeria

Abstract

The aim of this work is to analyze the dynamic behavior of axially loaded Timoshenko flexible shafts with cantilevered overhung disk based on the differential transformation analysis. The equations of motion are derived using Hamilton’s principle. The set of the latter consists of four coupled partial differential equations, which can be reduced to a set of two coupled equations by using a complex transformation to further improve the computational effort. An efficient mathematical recursive technique called the differential transformation method (DTM) is then used to solve the differential equations of motion. The natural frequencies of the shaft are obtained, the influence of intrinsic and extrinsic parameters on the natural frequencies is investigated, and the results are compared to those found in the literature. The results reflect the high accuracy and precision of the DTM. The novelty of the work is the application of the DTM to determine the frequency characteristics and the stability of an axially loaded overhung rotor’s free vibration analysis. These results show that the current analysis is accurate and offers an effective approach that is relatively simple and more direct regarding previous modal analyses.

Publisher

World Scientific Pub Co Pte Ltd

Subject

Computer Science Applications,Mechanics of Materials,General Materials Science,Modeling and Simulation,Numerical Analysis

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Frequency design of a vertical cantilever beam carrying tip mass;International Journal of Structural Stability and Dynamics;2023-10-13

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