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- W2896023820 startingPage "JPRQQM" @default.
- W2896023820 abstract "Five-hole-probes are common use in turbomachinery flow investigations, even though, inserting a probe into a flow field inevitably induces perturbations to the flow which can falsify the measurement results, especially when exposed to transonic flows. The objective of the investigations presented here is to evaluate the Mach number measurements of a five-hole-probe (5HP) in the wake flow of a transonic turbine cascade at engine relevant Reynolds numbers by comparing them to the results of particle image velocimetry (PIV). Furthermore, PIV measurements were performed with inserted probe to investigate the influence of the probe on the wake flow field. Together with a sensitivity study of 5HP measurements in flow regimes close to Ma = 1, the results demonstrate how the measurement uncertainty can be improved in high subsonic flow regimes." @default.
- W2896023820 created "2018-10-26" @default.
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- W2896023820 date "2018-10-08" @default.
- W2896023820 modified "2023-10-06" @default.
- W2896023820 title "On the challenge of five-hole-probe measurements at high subsonic Mach numbers in the wake of transonic turbine cascades" @default.
- W2896023820 cites W1979596412 @default.
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- W2896023820 doi "https://doi.org/10.22261/jgpps.jprqqm" @default.
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