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Experimental Analysis of a Waveguide Pressure Measuring System

J. Eng. Gas Turbines Power  -- April 2010 --  Volume 132,  Issue 4, 041603 (7 pages)
doi:10.1115/1.3159387

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Author(s):
Matthew A. White, Manuj Dhingra, and J. V. R. Prasad
Compressor Research Laboratory, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332
An infinite-line probe is commonly used to measure unsteady pressure in high-temperature environments while protecting the pressure transducer. In this study, an existing theoretical model is used to derive the response of a waveguide pressure measuring system. An ambient temperature centrifugal compressor rig acts as an experimental source of fluctuating pressure. The compressor is operated at different discrete rotational speeds, and the blade-passing frequencies are used to obtain frequency response data. In the experiments, pressure waves attenuated at a rate faster than that predicted by the theoretical model for a 0.322 m (12 in.) sensor offset. Furthermore, the decay in the magnitude of the pressure oscillations accelerated at blade-passing frequencies above 9 kHz. A unique contribution of this study is to show that whereas the experimentally observed overall attenuation is broadly consistent with the theoretical predictions, pressure oscillations corresponding to individual blade passages may be disproportionally attenuated.

©2010 American Society of Mechanical Engineers

History: Received 24 March 2009; revised 7 April 2009; published 26 January 2010
doi: http://dx.doi.org/10.1115/1.3159387

KEYWORDS and PACS

Keywords
PACS
  • 89.20.Kk
    Engineering
  • 89.40.Dd
    Air transportation
  • 89.20.Bb
    Industrial and technological research and development
  • YEAR: 2010

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PUBLICATION DATA

Coden:
JETPEZ
ISSN:
0742-4795 (print)   1528-8919 (online)
Publisher:
AIP is a member of CrossRef ASME

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