3-D Inviscid Analysis of Radial Turbine Flow

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3-D Inviscid Analysis of Radial Turbine Flow ( 3-d-inviscid-analysis-radial-turbine-flow )

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2. Anderson, D.A., Tannehill, J.C., and.-Pletcher, R.H-., Computational Fluid Mechanics.and Heat Transfer,.Hemisphere Publishing Co., Washington, 1984. 3. Katsanis, T., "Calculation of Three-Dimensional Viscous Flow Through Turbomachinery Blade Passages by Parabolic Marching," AIAA Paper 85-1408, July 1985. 4. Denton, J.D., "ATime Marching Method for Two- and Three-Dimensional Blade to Blade Flow," ARC-R.&M.-3775, Aeronautical Research Council, London, 1975. 5. Denton, J.D. and Singh, U.K., "Time Marching Methods for Turbomachinery Flow Calculation," Application of Numerical Methods to Flow Calculations inTurbomachines, VKI-LEC-SER-1979-7, Von Karman Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium, 1979. 6. Denton, J.D., "An Improved Time Marching Method for Turbomachinery Flow Calculation," Journal of Engineering for Power, Vol. 105, No. 3, July 1983, pp. 514-524. 7. Denton, J.D., "AMethod of Calculating Fully Three-Dimensional Inviscid Flow Through Any Type of Turbomachine Blade Row," Aerothermodynamics of Low Pressure Steam Turbines and Condensers, Vol. 1, VKI-LS-1983-06-VOL-1, Von Karman Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium, 1983. 8. Povinelli, L.A., "Assessment of Three-Dimensional Inviscid Codes and Loss Calculations for Turbine Aerodynamic Computations," Journal of Engineering for Gas Turbines and Power, Vol. 107, No. 2, Apr. 1985, pp. 265-276. 9. Goldman, L.J.; and Seasholtz, R.G., "Laser Anemometer Measurements in an Annular Cascade of Core Turbine Vanes and Comparison with Theory," NASA TP-2018, 1982. 10. Schwab, J.R., Stabe, R.G., and Whitney, W.J., "Analytical and Experimental Study of Flow Through an Axial Turbine Stage with a Nonuniform Inlet Radial Temperature Profile," AIAA Paper 83-1175, June 1983. 11. McLallin, K.L.; and Haas, J.E., "Experimental Performance and Analysis of 15.04-cm-tip-diameter, Radial-inflow Turbine with Work Factor of 1.126 and Thick Blading," NASA TP-1730, 1980. 12. Bosman, C.; and Highton, J., "ACalculation Procedure for Three-Dimensional, Time-Dependent, Inviscid, Compressible Flow Through Turbomachine Blades of Any Geometry," Journal of Mechanical Engineering Science, Vol. 21, No. 1, Feb. 1979, pp. 39-49. 13. Glassman, A.J.; and Wood, J.R., "Input Generator for Denton Three-Dimensional Turbomachine-Blade-Row Analysis Code," NASA TM-83324, 1983. 9

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