Unsteady three-dimensional multistage calculations are performed for a highly loaded, high-speed axial compressor to investigate the impact of real geometry modeling and different numerical approaches on the accuracy of the performance prediction. First, two features of the real geometries are separately compared with the calculation which consists of a pure flow path model except that rotor tip clearances are considered. One treats leakage generated by part gaps between variable stator vanes and the annulus lines. Another incorporates seal cavities to model leakage underneath the shrouded stators. Then, the influence of different numerical approach with different turbulence models is also investigated. Discussion on the impact of the CFD modeling on the performance prediction focuses on the prediction accuracies of stage operating points and spanwise mixing. It is suggested that a realistic simulation of turbulent-type flow unsteadiness in a multistage machine is important for an accurate prediction of spanwise mixing phenomena.
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ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5467-9
PROCEEDINGS PAPER
CFD Modeling Effects on Unsteady Multistage Simulation for a Transonic Axial Compressor
Hidekazu Kodama,
Hidekazu Kodama
IHI Corporation, Tokyo, Japan
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Naoki Tsuchiya,
Naoki Tsuchiya
IHI Corporation, Tokyo, Japan
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Yasuo Horiguchi,
Yasuo Horiguchi
Advanced Science & Intelligence Research Institute Corporation, Tokyo, Japan
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Junichi Kazawa
Junichi Kazawa
Japan Aerospace Exploration Agency, Tokyo, Japan
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Mai Yamagami
IHI Corporation, Tokyo, Japan
Hidekazu Kodama
IHI Corporation, Tokyo, Japan
Dai Kato
IHI Corporation, Tokyo, Japan
Naoki Tsuchiya
IHI Corporation, Tokyo, Japan
Yasuo Horiguchi
Advanced Science & Intelligence Research Institute Corporation, Tokyo, Japan
Junichi Kazawa
Japan Aerospace Exploration Agency, Tokyo, Japan
Paper No:
GT2011-46198, pp. 1689-1702; 14 pages
Published Online:
May 3, 2012
Citation
Yamagami, M, Kodama, H, Kato, D, Tsuchiya, N, Horiguchi, Y, & Kazawa, J. "CFD Modeling Effects on Unsteady Multistage Simulation for a Transonic Axial Compressor." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 7: Turbomachinery, Parts A, B, and C. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 1689-1702. ASME. https://doi.org/10.1115/GT2011-46198
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