This paper presents a description of Detached Eddy Simulations being carried out on a variable stator vane with a penny-cavity in order to determine the secondary flow phenomena in the main flowpath. Variable stator vanes are common in multi-stage compressors to prevent flow separations on rotor and stator blades at off-design operation points. The bearing of the stators at hub and tip generate unavoidable circular-shaped ring gaps, which are called penny-cavities. The aim of this paper is to determine secondary flow phenomena in variable stator vanes on an annular cascade testbed resulting from the throughflow of the penny-cavities. Reynolds-Averaged-Navier-Stokes simulations and scale resolving Detached-Eddy-Simulations of a variable stator vane with hub penny-cavity were therefore performed using Ansys CFX. The results of these simulations will be compared to corresponding simulations without penny-cavity. The study shows secondary flow phenomena, which are comparable to the interaction of a transverse jet in a free stream. Due to the low momentum ratio of R = 0.5, the jet immediately veers in the direction of the main flow. The typical vortices which develop from a transverse jet in a free stream are identified. The steady RANS simulation shows an asymmetrical counter-rotating vortex pair. A lack of unsteady secondary flow interaction can be seen in the RANS simulations in contrast to the Detached-Eddy-Simulations, which resolve large turbulent scales. Hence an interaction between the counter-rotating vortex pair and the unsteady shear layer vortices in the stator is visible. In the Detached Eddy Simulations the counter-rotating vortex pair is superimposed by the unsteady shear-layer vortices. The vortices produce significant additional mixing losses, which will be shown in detail. By comparing simulations with and without penny-cavity, the penny-cavity losses are quantified. In conclusion, this paper will help design engineers become more aware of the significance of the penny-cavity with variable stator vanes.
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ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
June 26–30, 2017
Charlotte, North Carolina, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5078-7
PROCEEDINGS PAPER
Secondary Flow in Variable Stator Vanes With Penny-Cavities Available to Purchase
Simon Stummann,
Simon Stummann
RWTH Aachen University, Aachen, Germany
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Daniel Pohl,
Daniel Pohl
RWTH Aachen University, Aachen, Germany
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Peter Jeschke,
Peter Jeschke
RWTH Aachen University, Aachen, Germany
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Hannes Wolf,
Hannes Wolf
MTU Aero Engines AG, München, Germany
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Alexander Halcoussis,
Alexander Halcoussis
MTU Aero Engines AG, München, Germany
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Matthias Franke
Matthias Franke
MTU Aero Engines AG, München, Germany
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Simon Stummann
RWTH Aachen University, Aachen, Germany
Daniel Pohl
RWTH Aachen University, Aachen, Germany
Peter Jeschke
RWTH Aachen University, Aachen, Germany
Hannes Wolf
MTU Aero Engines AG, München, Germany
Alexander Halcoussis
MTU Aero Engines AG, München, Germany
Matthias Franke
MTU Aero Engines AG, München, Germany
Paper No:
GT2017-63771, V02AT39A018; 12 pages
Published Online:
August 17, 2017
Citation
Stummann, S, Pohl, D, Jeschke, P, Wolf, H, Halcoussis, A, & Franke, M. "Secondary Flow in Variable Stator Vanes With Penny-Cavities." Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. Volume 2A: Turbomachinery. Charlotte, North Carolina, USA. June 26–30, 2017. V02AT39A018. ASME. https://doi.org/10.1115/GT2017-63771
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