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Numerical Analysis of an Instrumented Turbine Blade Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: 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 ...
Application of an Immersed Boundary Method on an Instrumented Turbine Blade With Large Eddy Simulation
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Leading edge instrumentation used in compressor and turbine blades for jet-engine test rigs can cause significant obstruction and lead to a marked increase in downstream pressure loss. Typical instrumentation used in such ...
Numerical Analysis of an Instrumented Turbine Blade Cascade
Publisher: American Society of Mechanical Engineers (ASME)
Abstract: 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 ...