Affiliation:
1. Universität Stuttgart, W. Germany
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.
Publisher
American Society of Mechanical Engineers
Cited by
6 articles.
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