000139207 001__ 139207
000139207 005__ 20190316234600.0
000139207 0247_ $$2doi$$a10.5293/IJFMS.2009.2.4.353
000139207 037__ $$aARTICLE
000139207 269__ $$a2009
000139207 260__ $$c2009
000139207 336__ $$aJournal Articles
000139207 520__ $$aIn the process of turbine modernizations, the investigation of the influences of water passage roughness on radial flow machine performance is crucial and validates the efficiency step up between reduced scale model and prototype. This study presents the specific losses per component of a Francis turbine, which are estimated by CFD simulation. Simulations are performed for different water passage surface roughness heights, which represents the equivalent sand grain roughness height. As a result, the boundary layer logarithmic velocity profile still exists for rough walls, but moves closer to the wall. Consequently, the wall friction depends not only on roughness height but also on its shape and distribution. The specific losses are determined by CFD numerical simulations for every component of the prototype, taking into account its own specific sand grain roughness height. The model efficiency step up between reduced scale model and prototype value is finally computed by the assessment of specific losses on prototype and by evaluating specific losses for a reduced scale model with smooth walls. Furthermore, surveys of rough walls of each component were performed during the geometry recovery on the prototype and comparisons are made with experimental data from the EPFL Laboratory for Hydraulic Machines reduced scale model measurements. This study underlines that if rough walls are considered, the CFD approach estimates well the local friction loss coefficient. It is clear that by considering sand grain roughness heights in CFD simulations, its forms a significant part of the global performance estimation. The availability of the efficiency field measurements provides a unique opportunity to assess the CFD method in view of a systematic approach for turbine modernization step up evaluation. Moreover, this paper states that CFD is a very promising tool for future evaluation of turbine performance transposition from the model scale to the prototype.
000139207 6531_ $$aFrancis Turbine
000139207 6531_ $$aModel & Prototype Testing
000139207 6531_ $$aCFD Simulation
000139207 6531_ $$aEfficiency Step Up
000139207 700__ $$0243093$$g172125$$aMARUZEWSKI, Pierre
000139207 700__ $$0243100$$g176678$$aHASMATUCHI, Vlad
000139207 700__ $$0243096$$g105887$$aMOMBELLI, Henri-Pascal
000139207 700__ $$aBURGGRAEVE, Danny
000139207 700__ $$aIOSFIN, Jacob
000139207 700__ $$aFINNEGAN, Peter
000139207 700__ $$0241012$$g104417$$aAVELLAN, François
000139207 773__ $$j2$$tInternational Journal of Fluid Machinery and Systems$$k4$$q353-362
000139207 8564_ $$uhttp://www.ijfms.org/$$zURL
000139207 8564_ $$uhttps://infoscience.epfl.ch/record/139207/files/IJFMS_Map_Paper_Final.pdf$$zn/a$$s507907
000139207 909C0 $$xU10309$$0252135$$pLMH
000139207 909CO $$ooai:infoscience.tind.io:139207$$qGLOBAL_SET$$pSTI$$particle
000139207 917Z8 $$x148230
000139207 937__ $$aLMH-ARTICLE-2009-008
000139207 973__ $$rREVIEWED$$sPUBLISHED$$aEPFL
000139207 980__ $$aARTICLE