Flow Path Excitation Mechanisms for Turbomachine Blades

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


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.


Guide Vane Exciting Force Turbine Stage Flow Guide Stator Blade 
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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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