Development of A 2-D compressor streamline curvature code

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2006, Pages 1005-1014

  Templalexis, Ioannis ^a   Pachidis, Vassilios ^b   Pilidis, Pericles ^b   Kotsiopoulos, Petros ^a  

^a Dekeleia Air Base   (Greece)

^b CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

Compressor; Gas turbine; Modeling; Performance; Streamline curvature

Indexed keywords

CYCLE SIMULATION; FLOW FIELDS; STREAMLINE CURVATURE (SLC);

BOUNDARY LAYERS; COMPUTER SIMULATION; COMPUTER SOFTWARE; DATA FLOW ANALYSIS; GAS TURBINES; PARAMETER ESTIMATION;

COMPRESSORS;

EID: 33750825790     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90867     Document Type: Conference Paper

References (19)

1. Wu, C. H., Wolfenstein, L. 1949 "Application Of Radial Equilibrium Condition To Axial-flow Compressor And Turbine Design", NACA TN 1795.
2. Hamrick, J. K., Ginsburg, A., Osborn, W. M., 1951 "Method Of Analysis For Compressible Flow Through Mixed Flow Centrifugal Impellers Of Arbitrary Design." NACA Report 1082.
3. Wright, C., and Kovach, K., 1953 "Design Procedure And Limited Test Results For A High Solidity", 12-inch transonic impeller with axial discharge." NACA RM E53B09.
4. Giamati, G. C., and Finger, B., 1965 "Design Velocity Distribution In Meridional Plane. In Aerodynamic Design Of Axial-Flow Compressors", NASA SP-36, Chapter VIII.
5. Swan, W. C., 1958 "A Practical Method Of Predicting Transonic-Compressor Performance", Journal of Engineering for Power, Transactions of the ASME 83: pp 322-330.
6. Novak, R. A., 1967 "Streamline Curvature Computing Procedures For Fluid-Flow Problems", Journal of Engineering for Power, Transactions of the ASME 89: 478-490.
7. Lieblein S., 1965 "Chapter VI - Experimental Flow In Two-Dimensional Cascades", of "NASA SP 36 - Aerodynamic Design Of Axial Flow Compressors", Scientific and Technical Information Division, National Aeronautics and Space Administration, Washington DC.
8. Carter A. D. S., 1950 "The Low Speed Performance Of Related Aerofoils In Cascade", National Gas Turbine Establishment, Report No. R.55, September 1949, Re-printed by the Aeronautical Research Council, CP29.
9. Lieblein S., 1960 "Incidence And Deviation Angle Correlations For Compressor Cascades", Transactions of the ASME, Journal of Basic Engineering Vol. 82, pages 575-587.
10. Cetin M., Hirsch Ch., Serovy G. K. and UCER A. S., 1989 "An Off-Design Loss And Deviation Prediction Study For Transonic Axial Compressors", ASME Paper publication, ASME 89-GT-324, Presented at the 34th International Gas Turbine and Aeroengine Congress and Exposition, Toronto, Ontario, Canada, June.
11. Creveling H. F. and Carmody R. H., 1968 "Axial Flow Compressor Computer Program for Calculating Off-Design Performance (Program IV)", General Motors, Allison Division, Indianapolis, Prepared for NASA, Report CR-72427.
12. Aungier R. H., 2003 "Axial-Flow Compressors: A Strategy For Aerodynamic Design And Analysis", ASME Press, Three Park Avenue, New York, NY 10016, pp 204-207.
13. Barbosa J. R., "A Streamline Curvature Computational Program For Axial Compressor Performance Prediction", PhD Thesis, Volume 1, School of Mechanical Engineering, Cranfield Institute of Technology, pages 46-48, 1987.
14. Miller G. R., Lewis, G. W. and Hartmann M. J., 1961 "Shock Losses In Transonic Rotor Rows", Transactions of the ASME, Journal of Engineering for Power, Vol. 83, pages 235-242.
15. Jansen W. and Moffatt W. C., "The off-design analysis of axial flow compressors", Transactions of the ASME, Journal of Engineering for Power, Vol. 89, October 1967, pages 453-462.
16. Schwenk F. C., Lewis G. W. and Hartman M. J., 1957 "A preliminary analysis of the magnitude of shock losses in transonic compressors", NACA RM E57A30.
17. HOWELL A. R. 1945 "Fluid dynamics of axial compressors." Proc. I. Mech. E. 153: pp 441-82
18. GRIEPENTROG, H. R. "Secondary flow losses in axial compressors." AGARD LS 39, 1970
19. Urasek D. C., William T. G., Walter S. C., 1979, "Performance Of Two Stage Fan Having Low Aspect Ratio First Stage Rotor Blading.", NASA Technical Paper 1493.