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SUMMARY:Numerical analysis of instrumentation in aeroengines - Bryn Ubald\
 , CUED
DTSTART:20171110T130000Z
DTEND:20171110T140000Z
UID:TALK95278@talks.cam.ac.uk
CONTACT:Charlotte Coles
DESCRIPTION:The measurement accuracy of the temperature/pressure probe mou
 nted at the leading edge of a turbine/compressor blade is crucial for esti
 mating the fuel consumption of a turbo-fan engine. Apart from the measurem
 ent error itself\, the probe also introduces extra losses. This again woul
 d compromise the measurement accuracy of the overall engine efficiency. A 
 series of high-fidelity analysis have been conducted to understand the los
 s sources and behaviour of the flow in such an environment.
LOCATION:JDB Seminar Room\, CUED
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