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Development and Application of a High Frequency Wedge Probe FREE

[+] Author Affiliations
H. Bubeck, J. Wachter

Universität Stuttgart, W. Germany

Paper No. 87-GT-216, pp. V001T01A074; 8 pages
doi:10.1115/87-GT-216
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 1: Turbomachinery
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7923-8
  • Copyright © 1987 by ASME

abstract

To investigate the three dimensional unsteady flow behind rotating blade rows of turbomachines, a high response pressure probe has been developed. Surface mounted miniature pressure transducers are used to measure the flow fluctuations, while the mean pressures are measured simultaneously with adjacent conventional pressure lead tubes. The steady state and the dynamic behaviour of the probe were investigated. The application of the probe to the rotor exit flow of an axial compressor is described and results are presented.

Copyright © 1987 by ASME
Topics: Probes , Wedges
This article is only available in the PDF format.

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