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Appl. Sci. 2018, 8, 2038 15 of 16 Subscripts a axial direction b blade h hub location m meridional direction opt optimal value r radial direction rms root mean square value s shroud location 1 nozzle inlet, i.e., volute outlet 2 throat section of nozzle 3 exit section of nozzle 4 inlet section of rotor 5 throat section of rotor 6 exit section of rotor References 1. Rohlik, H.E.; Kofskey, M.G.; Katsanis, T. Summary of NASA radial turbine research related to Brayton cycle space power system. Presented at the 2nd Interagency Energy Conversion Engineering Conference, Miami Beach, FL, USA, 13–17 August 1967. 2. Bozza, F.; Bellis, V.D. Steady modeling of a turbocharger turbine for automotive engines. J. Eng. Gas Turbines Power 2014, 136, 011701. [CrossRef] 3. Rodgers, C. The characteristics of radial turbines for small gas turbines. Presented at the ASME Turbo Expo 2003: Power for Land, Sea, and Air, Atlanta, GA, USA, 16–19 June 2003. 4. Deng, Q.H.; Niu, J.F.; Mao, J.R.; Feng, Z.P. Experimental and numerical investigation on overall performance of a radial inflow turbine for 100 kW microturbine. Presented at the ASME Turbo Expo 2007: Power for Land, Sea, and Air, Montreal, QC, Canada, 14–17 May 2007. 5. Rohlik, H.E. Analytical Determination of Radial Inflow Turbine Design Geometry for Maximum Efficiency; TN D-4384; NASA: Washington, DC, USA, 1968. 6. Wasserbauer, C.A.; Glassman, A.J. FORTRAN Program for Predicting Off-Design Performance of Radial Inflow Gas Turbines; TN D-8063; NASA: Washington, DC, USA, 1975. 7. Rodgers, C.; Geiser, R. Performance of a high efficiency radial/axial turbine. J. Turbomach. 1987, 109, 151–154. [CrossRef] 8. Whitfield, A.; Baines, N.C. Chapter 3. In Design of Radial Turbomachines; Office of Scientific and Technical Information, U.S. Department of Energy: New York, NY, USA, 1990. 9. Ye, F.; Feng, Z.P. Non-dimensional preliminary design and optimization for radial inflow turbine. Gas Turbine Technol. 1998, 11, 28–31. 10. Ebaid, M.S.Y.; Bhinder, F.S.; Khdairi, G.H. A unified approach for designing a radial flow gas turbine. J. Turbomach. 2003, 125, 598–606. [CrossRef] 11. Mistry, C.S.; Channiwala, S.A. Design of nozzle-less radial inflow gas turbine for small capacity (20kW) gas turbine engine. Presented at the ASME 2004 International Mechanical Engineering Congress and Exposition, Anaheim, CA, USA, 13–19 November 2004. 12. Feng, Z.P.; Deng, Q.H.; Li, J. Aerodynamic design and numerical simulation of radial inflow turbine impeller for a 100kW microturbine. Presented at the ASME Turbo Expo 2005: Power for Land, Sea, and Air, Reno, NV, USA, 6–9 June 2005. 13. Deng, Q.H. Design and Development, Aerodynamic Performance Test, and Tip Clearance Flow Characteristics of a Radial Inflow Turbine for 100 kW Microturbines. Ph.D. Thesis, Xi’an Jiaotong University, Xi’an, China, December 2008. 14. Suhrmann, J.F.; Peitsch, D.; Gugau, M.; Heuer, T.; Tomm, U. Validation and development of loss models for small size radial turbines. Presented at the ASME Turbo Expo 2010: Power for Land, Sea, and Air, Glasgow, UK, 14–18 June 2010.PDF Image | Design and Optimization Approach for Radial Inflow Turbines
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