0
RESEARCH PAPERS

The Design of Rotor Blades Taking Into Account the Combined Effects of Vibratory and Thermal Loads

[+] Author and Article Information
R. Bahree, A. M. Sharan

Memorial University of Newfoundland, St. John’s, Newfoundland, Canada A1B 3X5

J. S. Rao

Dept. of Mechanical Engineering, I.I.T., Hauz Khas, New Delhi, India

J. Eng. Gas Turbines Power 111(4), 610-618 (Oct 01, 1989) (9 pages) doi:10.1115/1.3240297 History: Received May 12, 1988; Online October 15, 2009

Abstract

The present work involves the design of rotor blades based on the thermal as well as centrifugal and nozzle excitation forces in the transient state. The finite element analysis has been used to calculate these stresses. The nozzle excitation forces have been modeled as a series of impulses occurring at instants of time known from the solution of kinematic equations.

Copyright © 1989 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

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