This paper describes the development and validation steps of a characteristics-based explicit along with a novel fully implicit mixing plane implementation for turbomachinery applications. The framework is an unstructured 3D RANS in-house modified solver, based on open-source libraries. Particular attention was paid to mass-conservation, accurate variables interpolation, and algorithm stability in order to improve robustness and convergence. By introducing a specific interface, allowing the use of algebraic multigrid solvers together with multiprocessor computation, a speed up of the numerical solution procedure was achieved. The validation of both mixing plane algorithms is carried out on an industrial radial compressor and a cold air 1.5 stages axial turbine.
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Engineering and Architecture,
Horw 6048,
e-mail: lucian.hanimann@hslu.ch
Engineering and Architecture,
Horw 6048,
Engineering and Architecture,
Horw 6048,
Postfach 2602
Zurich 8021,
Postfach 2602
Zurich 8021,
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August 2014
Research-Article
Development of a Novel Mixing Plane Interface Using a Fully Implicit Averaging for Stage Analysis
Lucian Hanimann,
Engineering and Architecture,
Horw 6048,
e-mail: lucian.hanimann@hslu.ch
Lucian Hanimann
1
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
e-mail: lucian.hanimann@hslu.ch
1Corresponding author.
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Luca Mangani,
Engineering and Architecture,
Horw 6048,
Luca Mangani
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
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Ernesto Casartelli,
Engineering and Architecture,
Horw 6048,
Ernesto Casartelli
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
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Thomas Mokulys,
Postfach 2602
Zurich 8021,
Thomas Mokulys
MAN Diesel and Turbo Schweiz AG
,Hardstrasse 319
,Postfach 2602
Zurich 8021,
Switzerland
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Sebastiano Mauri
Postfach 2602
Zurich 8021,
Sebastiano Mauri
MAN Diesel and Turbo Schweiz AG
,Hardstrasse 319
,Postfach 2602
Zurich 8021,
Switzerland
Search for other works by this author on:
Lucian Hanimann
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
e-mail: lucian.hanimann@hslu.ch
Luca Mangani
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
Ernesto Casartelli
Lucerne University of Applied Sciences and Arts
,Engineering and Architecture,
Technikumstrasse 21
,Horw 6048,
Switzerland
Thomas Mokulys
MAN Diesel and Turbo Schweiz AG
,Hardstrasse 319
,Postfach 2602
Zurich 8021,
Switzerland
Sebastiano Mauri
MAN Diesel and Turbo Schweiz AG
,Hardstrasse 319
,Postfach 2602
Zurich 8021,
Switzerland
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received November 27, 2013; final manuscript received December 14, 2013; published online January 31, 2014. Editor: Ronald Bunker.
J. Turbomach. Aug 2014, 136(8): 081010 (14 pages)
Published Online: January 31, 2014
Article history
Received:
November 27, 2013
Revision Received:
December 14, 2013
Citation
Hanimann, L., Mangani, L., Casartelli, E., Mokulys, T., and Mauri, S. (January 31, 2014). "Development of a Novel Mixing Plane Interface Using a Fully Implicit Averaging for Stage Analysis." ASME. J. Turbomach. August 2014; 136(8): 081010. https://doi.org/10.1115/1.4026323
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