Prediction of Axial-Flow Turbomachine Performance by Blade-Element Methods

[+] Author and Article Information
G. K. Serovy, J. C. Lysen

Department of Mechanical Engineering, Iowa State University, Ames, Iowa

J. Eng. Power 85(1), 1-6 (Jan 01, 1963) (6 pages) doi:10.1115/1.3675208 History: Received August 01, 1961; Online January 10, 2012


The blade-element method has been used effectively in the solution of the design problem for axial-flow turbomachines. A considerable body of data has been acquired to support the use of this system. The method has been applied in the investigation reported in this paper to the performance-prediction problem for blade rows in incompressible and compressible flows. Radial distributions of velocity and fluid properties were determined by numerical solution of the radial equilibrium condition, with radial entropy gradients included by using blade-element losses estimated from available experimental information. The effect of a loss gradient on the predicted performance of a typical axial-flow pump configuration is indicated and, for the case of an axial-flow compressor rotor operating in air, performance predicted is compared with experimentally measured performance.

Copyright © 1963 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