University of Cambridge > > Fluid Mechanics (CUED) > Numerical analysis of instrumentation in aeroengines

Numerical analysis of instrumentation in aeroengines

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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 Fluid Mechanics (CUED) series.

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