A grid-free numerical scheme is provided for the solution of unsteady flow in the hydraulic turbines. The Lagrangian vortex method is utilized to evaluate the convection and stretch of the vorticity, and the boundary element method is used to solve the Neumann problem to define the potential flow. The no-slip boundary condition is satisfied by generating vortex sticks at the solid surface. A semi-analytical regularization technique is applied to evaluate the singular boundary surface integrals of the potential velocity and its gradients accurately. The fast multipole method (FMM) has been extended to evaluate the velocity and velocity gradients induced by the discretized vortex blobs in the Lagrangian vortex method. The successful simulation for the unsteady flow through a hydraulic turbine’s runner has manifested the effectiveness of the proposed method.
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ASME-JSME-KSME 2011 Joint Fluids Engineering Conference
July 24–29, 2011
Hamamatsu, Japan
Conference Sponsors:
- Fluids Engineering Division
ISBN:
978-0-7918-4440-3
PROCEEDINGS PAPER
Numerical Simulation of Unsteady Flows Through a Francis Turbine Runner Using Vortex Methods
Baoshan Zhu,
Baoshan Zhu
Tsinghua University, Beijing, China
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Longbu Wang,
Longbu Wang
Tsinghua University, Beijing, China
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Shuliang Cao
Shuliang Cao
Tsinghua University, Beijing, China
Search for other works by this author on:
Baoshan Zhu
Tsinghua University, Beijing, China
Longbu Wang
Tsinghua University, Beijing, China
Jie Zhai
Tsinghua University, Beijing, China
Shuliang Cao
Tsinghua University, Beijing, China
Paper No:
AJK2011-05009, pp. 1751-1761; 11 pages
Published Online:
May 25, 2012
Citation
Zhu, B, Wang, L, Zhai, J, & Cao, S. "Numerical Simulation of Unsteady Flows Through a Francis Turbine Runner Using Vortex Methods." Proceedings of the ASME-JSME-KSME 2011 Joint Fluids Engineering Conference. ASME-JSME-KSME 2011 Joint Fluids Engineering Conference: Volume 1, Symposia – Parts A, B, C, and D. Hamamatsu, Japan. July 24–29, 2011. pp. 1751-1761. ASME. https://doi.org/10.1115/AJK2011-05009
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