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About OMICS Group OMICS Group International is an amalgamation of Open Access publications and worldwide international science conferences and events. Established in the year 2007 with the sole aim of making the information on Sciences and technology ‘Open Access’, OMICS Group publishes 400 online open access scholarly journals in all aspects of Science, Engineering, Management and Technology journals. OMICS Group has been instrumental in taking the knowledge on Science & technology to the doorsteps of ordinary men and women. Research Scholars, Students, Libraries, Educational Institutions, Research centers and the industry are main stakeholders that benefitted greatly from this knowledge dissemination. OMICS Group also organizes 300 International conferences annually across the globe, where knowledge transfer takes place through debates, round table discussions, poster presentations, workshops, symposia and exhibitions.Open Access publicationsscholarly journalsInternational conferences
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About OMICS Group Conferences OMICS Group International is a pioneer and leading science event organizer, which publishes around 400 open access journals and conducts over 300 Medical, Clinical, Engineering, Life Sciences, Pharma scientific conferences all over the globe annually with the support of more than 1000 scientific associations and 30,000 editorial board members and 3.5 million followers to its credit. OMICS Group has organized 500 conferences, workshops and national symposiums across the major cities including San Francisco, Las Vegas, San Antonio, Omaha, Orlando, Raleigh, Santa Clara, Chicago, Philadelphia, Baltimore, United Kingdom, Valencia, Dubai, Beijing, Hyderabad, Bengaluru and Mumbai.
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Oct. 05, 2015 Won-Seok Heo Turbo System & Control Laboratory Institute of Advanced Machines and Design(IAMD) School of Mechanical and Aerospace Engineering Seoul National University Design and Performance Prediction of Centrifugal Compressor Mech – Aero 2015 - Aerodynamics -
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Turbo System and Control Laboratory, Seoul National University 3 Introduction Research Objective and Numerical Method Validation of CFD calculation results Analysis & Prediction model Conclusions Contents
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Turbo System and Control Laboratory, Seoul National University 4 Centrifugal compressor
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Turbo System and Control Laboratory, Seoul National University 5 Research subject 01 2 4 3 5 Volute exit 8 Diffuser vane Impeller blade Shroud Hub 1.1
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Turbo System and Control Laboratory, Seoul National University 6 Simulation Condition Type Tool Single PassageFull Passage Grid CFX Turbo Grid CFX Turbo Grid / ICEM Total nodes120k2200k Solver ToolANSYS CFX 11.0 Turbulence modelk-ε RANS Simulation typeSteady Boundary condition Inlet Total pressure Total temperature Flow angle OutletMass flow rate InterfaceMixing plane
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Turbo System and Control Laboratory, Seoul National University 7 Validation of CFD result
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Turbo System and Control Laboratory, Seoul National University 8 Performance map ●
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Turbo System and Control Laboratory, Seoul National University 9 Impeller choking near shroud(0.9span) ; Mu=1.10, ϕ =0.158 Shock wave 1.1 1.45
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Turbo System and Control Laboratory, Seoul National University 10 Impeller Performance ; Work coefficient
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Turbo System and Control Laboratory, Seoul National University 11 Flow chart ; Work coefficient Prediction model
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Turbo System and Control Laboratory, Seoul National University 12 Flow angle function of flow coefficient at impeller exit
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Turbo System and Control Laboratory, Seoul National University 13 Flow angle function of flow coefficient at impeller exit
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Turbo System and Control Laboratory, Seoul National University 14 1D equation for predicting work coefficient
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Turbo System and Control Laboratory, Seoul National University 15 Flow angle function of flow coefficient at impeller exit
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Turbo System and Control Laboratory, Seoul National University 16 Flow angle function of flow coefficient at impeller exit
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Turbo System and Control Laboratory, Seoul National University 17 1D equation for predicting work coefficient
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Turbo System and Control Laboratory, Seoul National University 18
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Turbo System and Control Laboratory, Seoul National University 19 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 20 MuA(Intercept)BC 0.8428304.923436.26-94.0204 0.9-6.42E+0559452.49-330.27 1.03113249-7.01E+06247965.3-1636.95 1.1-1.59E+07500285.9-3371.06 1.15-2.46E+07737054.4-4953.38 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 21 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 22 Flow coefficient correlation & Prediction of work coefficient
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Turbo System and Control Laboratory, Seoul National University 23 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 24 MuA(Intercept)BC 0.8-57763.37738278.95-208.191 0.9-1.26E+0677309.94-460.208 1.03113249-7.16E+06249087.7-1623.32 1.1-1.34E+07421370.7-2771.21 1.15-1.76E+07532723-3461.57 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 25 Reynolds number function of flow angle at impeller exit
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Turbo System and Control Laboratory, Seoul National University 26 Flow coefficient correlation & Prediction of work coefficient
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Turbo System and Control Laboratory, Seoul National University 27 Centrifugal compressor - Centrifugal compressor(Z v =12) data analysis - Imp.-diff. matching correlation of the number of vanes Vaned diffuser - Calculation of diverse vaned diffusers( ξ =70 ° ) by CFD - Investigation of design parameters Accumulation of data base : CFD(by SNU), test(by STW) Development of the in-house program(by MATLAB) - 1D aerodynamic design model - Performance prediction model conclusion
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Turbo System and Control Laboratory, Seoul National University 28 Thank you for your attention.
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Turbo System and Control Laboratory, Seoul National University 29 Solidity
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