Large eddy simulations validated with the aid of direct numerical simulation (DNS) are used to study the concerted action of reduced frequency and flow coefficient on the performance of the T106A low-pressure turbine profile. The simulations are carried out by using a discretization in space and time that allows minimizing the accuracy loss with respect to DNS. The reference Reynolds number is 100,000, while reduced frequency and flow coefficient cover a range wide enough to provide valid qualitative information to designers. The various configurations reveal differences in the loss generation mechanism that blends steady and unsteady boundary layer losses with unsteady wake ingestion losses. Large values of the flow coefficient can alter the pressure side unsteadiness and the consequent loss generation. Low values of the flow coefficient are associated with wake fogging and reduced unsteadiness around the blade. The reduced frequency further modulates these effects. The simulations also reveal a clear trend of losses with the wake path, discussed by conducting a loss-breakdown analysis that distinguishes boundary layer from wake distortion losses.
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November 2016
Research-Article
High-Fidelity Simulations of Low-Pressure Turbines: Effect of Flow Coefficient and Reduced Frequency on Losses
V. Michelassi,
V. Michelassi
General Electric Global Research,
Garching bei München D-85748, Germany
e-mail: vittorio.michelassi@ge.com
Garching bei München D-85748, Germany
e-mail: vittorio.michelassi@ge.com
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L. Chen,
L. Chen
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Search for other works by this author on:
R. Pichler,
R. Pichler
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
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R. Sandberg,
R. Sandberg
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
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R. Bhaskaran
R. Bhaskaran
General Electric Global Research,
Niskayuna 12309, NY
Niskayuna 12309, NY
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V. Michelassi
General Electric Global Research,
Garching bei München D-85748, Germany
e-mail: vittorio.michelassi@ge.com
Garching bei München D-85748, Germany
e-mail: vittorio.michelassi@ge.com
L. Chen
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
R. Pichler
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
R. Sandberg
Aerodynamics and Flight Mechanics
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
Research Group, Faculty of Engineering
and the Environment,
University of Southampton,
Southampton SO17 1BJ, UK
R. Bhaskaran
General Electric Global Research,
Niskayuna 12309, NY
Niskayuna 12309, NY
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received February 10, 2016; final manuscript received March 1, 2016; published online May 17, 2016. Editor: Kenneth C. Hall.
J. Turbomach. Nov 2016, 138(11): 111006 (12 pages)
Published Online: May 17, 2016
Article history
Received:
February 10, 2016
Revised:
March 1, 2016
Citation
Michelassi, V., Chen, L., Pichler, R., Sandberg, R., and Bhaskaran, R. (May 17, 2016). "High-Fidelity Simulations of Low-Pressure Turbines: Effect of Flow Coefficient and Reduced Frequency on Losses." ASME. J. Turbomach. November 2016; 138(11): 111006. https://doi.org/10.1115/1.4033266
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