>
Fa   |   Ar   |   En
   Effect of Di erent Geometries in Simulation of 3D Viscous Flow in Francis Turbine Runners.  
   
نویسنده Firoozabadi B. ,Dadfar R. ,Pirali A. P. ,Ahmadi G.
منبع scientia iranica - 2009 - دوره : 16 - شماره : 4 - صفحه:363 -369
چکیده    Overall turbine analysis requires large cpu time and computer memory, even in the present days. as a result, choosing an appropriate computational domain accompanied by a suitable boundary condition can dramatically reduce the time cost of computations. this work compares different geometries for numerical investigation of the 3d flow in the runner of a francis turbine, and presents an optimum geometry with least computational effort and desirable numerical accuracy. the numerical results are validated with a gamm francis turbine runner, which was used as a test case (gamm workshop on 3d computation of incompressible internal flows, 1989) in which the geometry and detailed best efficiency measurements were publically accessible. in this simulation, the flow is assumed to be steady and the inlet boundary condition is prescribed using experimental data. the effect of turbulence is considered by the k -(epsilon) model. the present investigation demonstrates that consideration of 2-blade geometry with periodicboundary conditions is the best choice of computational domain. by 1-blade geometry, convergence of the numerical simulation is not appropriate, whereas 13-blade geometry leads to a coarse grid that canincrease inaccuracy and computational cost. finally, this paper presents a qualitative survey to forecast cavitation region inception which correlates satisfactorily with experimental observations.
کلیدواژه Numerical simulation; Francis turbine runner; GAMM; Viscous flow analysis.
آدرس sharif university of technology, Department of Mechanical Engineering , ایران, sharif university of technology, Department of Mechanical Engineering , ایران, sharif university of technology, Department of Mechanical Engineering , ایران, Clarkson University., Department of Mechanical and Aeronautical Engineering , USA.
پست الکترونیکی roozabadi@sharif.edu
 
     
   
Authors
  
 
 

Copyright 2023
Islamic World Science Citation Center
All Rights Reserved