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|Title:||Numerical study of the flow past an axial turbine stator casing and perspectives for its management|
|Authors:||Kadhim, Hakim K. T.|
Obaida, Hayder M. B.
Gostelow, J. Paul
|Presented at:||ASME Turbo Expo 2017: Turbine Technical Conference and Exposition, Charlotte, NC, USA|
|Publisher:||American Society of Mechanical Engieers ASME|
|Citation:||Proceedings of ASME Turbo Expo 2017: Turbine Technical Conference and Exposition IGTI 2017, 2017, pp. 1-13|
|Abstract:||The interaction of secondary flow with the main passage flow results in entropy generation; this accounts for considerable losses in turbomachines. Low aspect ratio blades in an axial turbine lead to a high degree of secondary flow losses. A particular interest is the reduction in secondary flow strength at the turbine casing, which adversely affects the turbine performance. This paper presents a selective review of effective techniques for improving the performance of axial turbines by turbine end wall modifications. This encompasses the use of axisymmetric and non-axisymmetric end wall contouring and the use of fences. Specific attention is given to non-axisymmetric end walls and to their effect on secondary flow losses. A baseline three-dimensional steady RANS k-ω SST model, with axisymmetric walls, is validated against experimental measurements from the Institute of Jet Propulsion and Turbomachinery at the Rheinisch-Westfälische Technische Hochschule (RWTH) Aachen, Germany, with comparative solutions generated by ANSYS Fluent and OpenFOAM. The predicted performance of the stator passage with an axisymmetric casing is compared with that from using a contoured casing with a groove designed using the Beta distribution function for guiding the groove shape. The prediction of a reduced total pressure loss coefficient with the application of the contoured casing supports the groove design approach based on the natural path of the secondary flow features. This work also provided an automated workflow process, linking surface definition in MATLAB, meshing in ICEM CFD, and flow solving and post-processing OpenFOAM. This has generated a casing contouring design tool with a good portability to industry, to design and optimize new turbine blade passages.|
|Embargo on file until:||1-Jan-10000|
|Rights:||Copyright © 2017, American Society of Mechanical Engieers ASME. All rights reserved.|
|Description:||The file associated with this record is under a permanent embargo in accordance with the publisher's policy. The full text may be available through the publisher links provided above.|
|Appears in Collections:||Conference Papers & Presentations, Dept. of Engineering|
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|20170302 ASME2017-63055.pdf||Post-review (final submitted author manuscript)||1.03 MB||Adobe PDF||View/Open|
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