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Flow Path Excitation Mechanisms for Turbomachine Blades

  • N. F. Rieger
Part of the International Centre for Mechanical Sciences book series (CISM, volume 297)

Abstract

The sources of non-steady forces in a turbine stage are reviewed. Procedures for line-vortex stage flow analysis and for actuator disk analyses are described, with details of analytical contributions to these areas. Experimental procedures for measurements of blade non-steady forces in the laboratory and in the field are described. Selected test data are included. Recent developments using the rotating water table approach are reviewed.

Keywords

Guide Vane Exciting Force Turbine Stage Flow Guide Stator Blade 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag Wien 1988

Authors and Affiliations

  • N. F. Rieger
    • 1
  1. 1.Stress Technology IncorporatedRochesterUSA

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