| Summary: | The three hole, wedge-type pneumatic pressure probe represents a robust
traverse probe design which is widely used for total and static pressure and yaw angle
measurements in turbomachinery. However, unsteady flows are incorrectly averaged due
to pneumatic meaning errors in the pressure pipes. Wedge probes also fail to measure the
correct static pressure when operating in close proximity to a wall through which the
probe is inserted. Thirdly, the aerodynamic calibration obtained for a wedge-type probe
in a closed wind tunnel differs appreciably from that obtained in an open jet. If not
corrected, these errors will corrupt any calculation of turbomachinery blade row
performance.
In this investigation, the second and third effects described above have been
addressed. A factorial experiment was completed in which the influence of seven
variables on the wall proximity effect was quantified. Flow visualisation studies were
performed to understand the responsible flow mechanisms. Two regions of re-circulating
flow were identified in the probe wake, the structure of which depended on the probe
immersion. Similar re-circulatory flows were resolved from three-dimensional
computational fluid dynamics (CFD) calculations of the flow over a wedge probe. A link
between the probe wake re-circulations and flow over the wedge faces was established.
Based on this understanding of the flow structures, a model was developed from which
the wall proximity effect could be predicted for a given set of conditions.
Wedge probe calibrations were completed in a closed wind tunnel and in two
open jets. Discrepancies in the static pressure coefficient and yaw angle sensitivity results
were found. These were partially explained in terms of modifications to the probe wake
structure which occurred when the probes were calibrated in the open jet facilities.
Procedures for correcting the wall proximity effect and for avoiding the facility
dependence of wedge probe calibrations were developed from this understanding of the
flow mechanisms involved.
Based on the findings of this investigation, a novel wedge probe was designed to
minimise the wall proximity effect. This probe demonstrated a reduction in the wall
proximity effect, from 20% dynamic head with current designs, to 3% dynamic head at
flows typical of high speed turbomachinery.
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