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Unsteady Velocity- and Turbulence Measurements With a Fast Response Pressure Probe FREE

[+] Author Affiliations
G. Ruck, H. Stetter

Universität Stuttgart, W. Germany

Paper No. 90-GT-232, pp. V001T01A079; 8 pages
doi:10.1115/90-GT-232
From:
  • ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Brussels, Belgium, June 11–14, 1990
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7904-7
  • Copyright © 1990 by ASME

abstract

To investigate the three-dimensional unsteady flow and the turbulence intensities behind rotating blade rows of turbomachines, a procedure using a fast-response pressure probe has been developed. The integration of the cylindrical miniature pressure transducers into the probe head minimizes the risk of mechanical damage. The dynamic behaviour of the probe was analyzed. The application of the probe to the rotor exit flow of an axial compressor is described and results are presented.

Copyright © 1990 by ASME
Topics: Pressure , Turbulence , Probes
This article is only available in the PDF format.

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