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n 1⁄4 rotor meridional velocity ratio [15] Jones, A. C., 1994, “Design and Test of a Small, High Pressure Ratio Radial Turbine,” ASME Paper No. 94-GT-135. [16] Glassman, A., 1994, “Design Analysis of Radial Inflow Turbines,” Technical Report, National Aeronautics and Space Administration, Lewis Research Cen- ter, Cleveland, OH, Report No. LEW-12684. [17] Suhrmann, J. F., Peitsch, D., Gugau, M., Heuer, T., and Tomm, U., 2010, “Validation and Development of Loss Models for Small Size Radial Turbines,” ASME Paper No. GT2010-22666. [18] Aungier, R. H. A., 2006, Turbine Aerodynamics: Axial-Flow and Radial-Inflow Tur- bine Design and Analysis, American Society of Mechanical Engineers, New York. [19] De Miranda Ventura, C. A., 2012, “Aerodynamic Design and Performance Estima- tion of Radial Inflow Turbines for Renewable Power Generation Applications,” Ph.D. thesis, The University of Queensland, Queensland, Australia. [20] Lemmon, E. W., Huber, M. L., and McLinden, M. O., 2012, “NIST Standard Refer- ence Database 23: Reference Fluid Thermodynamic and Transport Properties (REFPROP),” National Institute of Standards and Technology, Gaithersburg, MD. [21] Span, R., and Wagner, W., 1996, “A New Equation of State for Carbon Dioxide Covering the Fluid Region From the Triple-Point Temperature to 1100 K at Pressures Up to 800 MPA,” J. Phys. Chem. Ref. Data, 25(6), pp. 1509–1596. [22] Hiett, G. F., and Johnston, I. H., 1963, “Paper 7: Experiments Concerning the Aerodynamic Performance of Inward Flow Radial Turbines,” Institution of Mechanical Engineers, Conference Proceedings, Vol. 178, SAGE Publications, London, pp. 28–42. [23] Marscher, W., 1992, “Structural Analysis: Stresses Due to Centrifugal, Pressure and Thermal Loads in Radial Turbines,” VKI Lecture Series, Radial Turbines, von Karman Institute for Fluid Dynamics, Sint-Genesius-Rode, Belgium, Tech- nical Report No. 93. [24] Blevins, R. D., and Plunkett, R., 1980, “Formulas for Natural Frequency and Mode Shape,” ASME J. Appl. Mech., 47(2), pp. 461–462. [25] Korpela, S. A., 2012, Principles of Turbomachinery, Wiley, Hoboken, NJ. [26] Woolley, N., and Hatton, A., 1973, “Viscous Flow in Radial Turbomachine Blade Passages,” Conference on Heat and Fluid Flow in Steam and Gas Turbine Plant, Coventry, UK, Apr. 3–5, pp. 175–181. [27] Rohlik, H. E., 1968, “Analytical Determination of Radial Inflow Turbine Design Geometry for Maximum Efficiency,” National Aeronautics and Space Adminis- tration, Lewis Research Center; Cleveland, OH, Report No. NASA-TN-D-4384. [28] Somaya, K., Kishino, T., Miyatake, M., and Yoshimoto, S., 2014, “Static Char- acteristics of Small Aerodynamic Foil Thrust Bearings Operated Up to 350,000 r/min,” Proc. Inst. Mech. Eng. Part J, 228(9), pp. 928–936. [29] Swann, P., 2015 “Bearing Selection Calculation,” Queensland Geothermal Energy Centre of Excellence, The University of Queensland, Queensland, Aus- tralia, Report No. QGECE 23-01-CL-06. [30] Shepherd, D. G., 1956, Principles of Turbomachinery, Macmillan, New York. [31] Balje, O. E., 1981, Turbomachines: A Guide to Design, Selection, and Theory, Wiley, Toronto, Canada. [32] Futral, S. M., Jr., and Holeski, D. E., 1969, “Experimental Results of Varying the Blade-Shroud Clearance in a 6.02-Inch Radial-Inflow Turbine,” National Aeronautics and Space Administration, Lewis Research Center; Cleveland, OH, Report No. NASA-TN-D-5513. [33] Glassman, A. J., 1976, “Computer Program for Design Analysis of Radial- Inflow Turbines,” National Aeronautics and Space Administration, Lewis Research Center; Cleveland, OH, Report No. NASA-TN-D-8164. [34] Whitfield, A., and Wallace, F., 1973, “Study of Incidence Loss Models in Radial and Mixed-Flow Turbomachinery,” Conference on Heat and Fluid Flow in Steam and Gas Turbine Plant, Coventry, UK, Apr. 3–5, pp. 122–128. [35] Daily, J. W., and Nece, R. E., 1960, “Chamber Dimension Effects on Induced Flow and Frictional Resistance of Enclosed Rotating Disks,” ASME J. Basic Eng., 82(1), pp. 217–230. [36] Glassman, A. J., 1995, “Enhanced Analysis and Users Manual for Radial-Inflow Turbine Conceptual Design Code RTD,” National Aeronautics and Space Adminis- tration, Lewis Research Center; Cleveland, OH, Report No. NASA-CR-195454. [37] Ghosh, S. K., Sahoo, R., and Sarangi, S. K., 2011, “Mathematical Analysis for Off-Design Performance of Cryogenic Turboexpander,” ASME J. Fluids Eng., 133(3), p. 031001. [38] Futral, S. M., and Wasserbauer, C. A., 1965, “Off-Design Performance Predic- tion With Experimental Verification for a Radial-Inflow Turbine,” National Aeronautics and Space Administration, Washington, DC, Technical Report No. NASA-TN-D-2621. q ; q ; q 1⁄4 density, average density of working flow, density of m 3 materials (kg m ) rr, rY 1⁄4 elastic stress, yield stress (GPa) s 1⁄4 shear stress (kg m1 s2) u 1⁄4 flow coefficient w 1⁄4 head coefficient x 1⁄4 turbine rotor angular velocity (rad s1) xn 1⁄4 rotor blade natural frequency (Hz) Subscripts a 1⁄4 axial direction b 1⁄4 back face h 1⁄4 rotor hub section m 1⁄4 meridional component r 1⁄4 radial direction rms 1⁄4 root mean square t 1⁄4 rotor tip section, tangential component 0 1⁄4 stagnation state 4 1⁄4 rotor inlet section 6 1⁄4 rotor outlet section h 1⁄4 tangential component References [1] Parida, B., Iniyan, S., and Goic, R., 2011, “A Review of Solar Photovoltaic Technologies,” Renewable Sustainable Energy Rev., 15(3), pp. 1625–1636. [2] Mekhilef, S., Saidur, R., and Safari, A., 2011, “A Review on Solar Energy Use in Industries,” Renewable Sustainable Energy Rev., 15(4), pp. 1777–1790. [3] Harries, D. N., Paskevicius, M., Sheppard, D. A., Price, T. E. C., and Buckley, C. E., 2012, “Concentrating Solar Thermal Heat Storage Using Metal Hydrides,” Proc. IEEE, 100(2), pp. 539–549. [4] Dostal, V., 2004, “A Supercritical Carbon Dioxide Cycle for Next Generation Nuclear Reactors,” Ph.D. thesis, Massachusetts Institute of Technology, Cam- bridge, MA. [5] Feher, E. G., 1968, “The Supercritical Thermodynamic Power Cycle,” Energy Convers., 8(2), pp. 85–90. [6] Angelino, G., 1967, “Perspectives for the Liquid Phase Compression Gas Turbine,” ASME J. Eng. Gas Turbines Power, 89(2), pp. 229–236. [7] Angelino, G., 1968, “Carbon Dioxide Condensation Cycles for Power Production,” ASME J. Eng. Gas Turbines Power, 90(3), pp. 287–295. [8] Angelino, G., 1969, “Real Gas Effects in Carbon Dioxide Cycles,” ASME Paper No. 69-GT-102. [9] Zhang, H., Zhao, H., Deng, Q., and Feng, Z., 2015, “Aerothermodynamic Design and Numerical Investigation of Supercritical Carbon Dioxide Turbine,” ASME Paper No. GT2015-42619. [10] Turchi, C. S., Ma, Z., Neises, T. W., and Wagner, M. J., 2013, “Thermodynamic Study of Advanced Supercritical Carbon Dioxide Power Cycles for Concentrating Solar Power Systems,” ASME J. Sol. Energy Eng., 135(4), p. 041007. [11] Wright, S. A., Radel, R. F., Vernon, M. E., Rochau, G. E., and Pickard, P. S., 2010, “Operation and Analysis of a Supercritical CO2 Brayton Cycle,” Techni- cal Report, Sandia National Laboratories, Report. No. SAND2010-0171. [12] Kalra, C., Sevincer, E., Brun, K., Hofer, D., and Moore, J., 2014, “Development of High Efficiency Hot Gas Turbo-Expander for Optimized CSP Supercritical CO2 Power Block Operation,” 4th International Symposium-Supercritical CO2 Power Cycles, Pittsburgh, PA, Sept. 9–10. [13] Ventura, C. A., Jacobs, P. A., Rowlands, A. S., Petrie-Repar, P., and Sauret, E., 2012, “Preliminary Design and Performance Estimation of Radial Inflow Tur- bines: An Automated Approach,” ASME J. Fluids Eng., 134(3), p. 031102. [14] Moustapha, H., Zelesky, M. F., Baines, N. C., and Japikse, D., 2003, Axial and Radial Turbines, Vol. 2, Concepts NREC, White River Junction, VT. JournalofTurbomachinery AUGUST2017,Vol.139 / 081008-11 Downloaded From: http://turbomachinery.asmedigitalcollection.asme.org/pdfaccess.ashx?url=/data/journals/jotuei/936123/ on 04/05/2017 Terms of Use: http://www.asme.org/a View publication stats bPDF Image | S CO2 Radial Turbine Design as a Function of Turbine Size
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