Determination of Natural Frequency of Aerofoil Section Blades Using Finite Element Approach, Study of Effect of Aspect Ratio and Thickness on Natural Frequency

Authors

  • Kamlesh Purohit Rajasthan Technical University
  • Manish Bhandari Rajasthan Technical University

DOI:

https://doi.org/10.4186/ej.2013.17.2.51

Keywords:

Aerofoil, finite element method.

Abstract

In this paper an attempt has been made to calculate the natural frequencies of aerofoil section blades using the finite element method. The effect of varying the aspect ratio and thickness on the frequencies has also been studied. It is observed that by increasing the value of aspect ratio, the natural frequency in all the modes is increased. It is also concluded that, there is some optimum value of thickness at which the natural frequencies in different modes of vibration are minimum.

Downloads

Download data is not yet available.

Author Biographies

Kamlesh Purohit

Department of Mechanical Engineering, Rajasthan Technical University, Rawatbhata Road, Kota 324010, India

Manish Bhandari

Department of Mechanical Engineering, Rajasthan Technical University, Rawatbhata Road, Kota 324010, India

Downloads

Published In
Vol 17 No 2, Oct 29, 2012
How to Cite
[1]
K. Purohit and M. Bhandari, “Determination of Natural Frequency of Aerofoil Section Blades Using Finite Element Approach, Study of Effect of Aspect Ratio and Thickness on Natural Frequency”, Eng. J., vol. 17, no. 2, pp. 51-62, Oct. 2012.