Vibration Analysis of Turbomachinery Blades Using Dedicated Discretization and Twisted Beam Theory

[+] Author and Article Information
B. Downs

Department of Mechanical Engineering, Loughborough University of Technology, Loughborough, Leicestershire, England

J. Mech. Des 102(3), 574-578 (Jul 01, 1980) (5 pages) doi:10.1115/1.3254787 History: Received June 17, 1979; Online November 17, 2009


A method of discretizing the stiffness and mass properties of beam segments of turbine or compressor blades is presented. The theory encompasses both the modification of beam bending and torsional stiffnesses due to pretwist and the coupling of bending and torsional deformation with axial deformation occasioned by pretwist. Examples show that accurate prediction of vibration frequencies for blades possessing substantial pretwist can be obtained by discretization on to a quite modest number of degrees of freedom. Some comparisons of prediction accuracy with Finite Element and other methods are included.

Copyright © 1980 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In