Radial turbine preliminary design and performance prediction

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Radial turbine preliminary design and performance prediction ( radial-turbine-preliminary-design-and-performance-prediction )

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CONCLUSIONS This document represents an "RTGD" engineering tool that aims to get a fast design of a radial turbine. Loss models have been implemented to predict the radial turbine overall performance with a rotor geometry optimization. Despite limited data available in the literature, RTGD has been validated using a real radial turbine test case, in addition a code-to-code comparison has been made. In the cases examined it is known that the passage loss represents the highest loss. From the comparison with the NASA RIFTUD code, the RTGD tool has proved easier to use by providing more complete results. The generation of the rotor 3-D geometry is currently under development, to carry out a further optimization through CFD analysis. In conclusion, the tests carried out were useful to understand the RTGD reliability for a future application in the aerospace propulsion field. The latter one will be integrated into Concurrent Design Facility (CDF), aimed at design all different components of the entire rocket-engine. REFERENCES 1. Baines N.C., “Low Development in Radial Turbine Rotors”. THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS, 1996. 2. Todd C.A. and Futral S. M. Jr., “A FORTRAN IV program to estimate the off-design performance of radial inflow turbines”, NASA TN D-5059, (1969). 3. Futral S. M. Jr. and Wasserbauer C. A., “Off-design performance prediction with Experimental Verification for a Radial Inflow Turbine”, NASA TN D-2621, (1965). 4. Wasserbauer, C. A. and Glassman, A. J., “Fortran program for predicting off-design performance of radial- inflow turbines”, NASA TN D-8063, (1975). 5. Glassman, A. J., “RIFTUD Radial Inflow Turbine Design”, NASA TN D-8164, (1976) 6. Rohlik, H. E., “Analytical Determination of Radial Inflow Turbine Design Geometry for Maximum Efficiency,” NASA, Technical Report No. TN D-4384, 1968. 7. Meitner, P. L. and Glassman, A. J. “RTOD Radial Turbine Off-Design”, NASA TP 2199, (1983). 8. RTOD NASA https://software.nasa.gov/software/LEW-14060-1 for U.S. Release Only. 9. Jones, A. C., “Design and Test of a Small, High Pressure Ratio Radial Turbine,” Trans. ASME J. Turbomach., 118(2), pp. 362–370, 1996. 10. Alexander Ponomarenko, “RPA: Tool for Rocket Propulsion Analysis”, 2015. 11. Leto A., Bonfiglioli A., Preliminary Design of a Radial Turbine for Methane Expander Rocket Engine. 72nd Conference of the Italian Thermal Machines Engineering Association, ATI2017. Energy Procedia Volume 126, Pages 738–745, 2017. 12. H. Moustapha, M.F. Zelesky, N.C. Baines, D. Japikse, Axial and Radial Turbines, Concepts NREC, (2003). 13. Dambach, R.; Huntsman, I.; Hodson, H.P. “An experimental study of tip clearance flow in radial inflow turbine”. J. Turbomach. 121, 644–650, 1999. 14. Ghosh, S. K., Sahoo, R. K. and Sarangi, S, K., “Mathematical Analysis for Off-Design Performance of Cryogenic Turboexpander Trans”, ASME Journal of Fluids Eng. 133(3), p, 031001, 2011. 020097-9

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