Numerical analysis of instrumentation in aeroengines

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• Bryn Ubald, CUED
• Friday 10 November 2017, 13:00-14:00
• JDB Seminar Room, CUED.

If you have a question about this talk, please contact Charlotte Coles.

The measurement accuracy of the temperature/pressure probe mounted at the leading edge of a turbine/compressor blade is crucial for estimating the fuel consumption of a turbo-fan engine. Apart from the measurement error itself, the probe also introduces extra losses. This again would compromise the measurement accuracy of the overall engine efficiency. A series of high-fidelity analysis have been conducted to understand the loss sources and behaviour of the flow in such an environment.

This talk is part of the Engineering Fluids Group Seminar series.

This talk is included in these lists:

• Acoustics Lab Seminars
• Engineering Department Acoustics/Combustion Student seminars
• Engineering Fluids Group Seminar
• JDB Seminar Room, CUED

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