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Part of the book series: Applied Mathematical Sciences ((AMS,volume 158))

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Selected Bibiliography

  • I. H. Abbot, A. E. von Doenhoff. Theory of Wing Sections. Dover Publications, New York, 1959.

    Google Scholar 

  • J. Ackeret. Zum Entwurf dichtstehender Schaufelgitter. Schweizerische Bauzeitung, 120,9, 372–384, 1942.

    Google Scholar 

  • R. H. Aungier. Centrifugal Compressors. ASME Press, New York, 2000.

    Google Scholar 

  • G. K. Batchelor. An Introduction to Fluid Dynamics. Cambridge University Press, Cambridge, 1970.

    Google Scholar 

  • A. Bölcs, P. Suter. Transsonische Turbomaschinen. G. Braun, Karlsruhe, 1986.

    Google Scholar 

  • A. Busemann. Das Förderhöhenverhältnis radialer Kreiselpumpen mit logarithmisch-spiraligen Schaufeln. ZAMM, 8, 372–384, 1928.

    MATH  Google Scholar 

  • M. V. Casey. A Mean Line Prediction Method for Estimating the Performance Characteristics of an Axial Compressor Stage. C 264/87, Int. Conf. on Turbomachinery: Efficiency Prediction and Improvement, Inst. Mech. Engrs., Cambridge, 1987.

    Google Scholar 

  • T. Cebeci. An Engineering Approach to the Calculation of Aerodynamic Flows. Springer, Berlin, Heidelberg, New York, 1999.

    Google Scholar 

  • T. Cebeci, J. Cousteix. Modeling and Computation of Boundary Layer Flows: Laminar, Turbulent and Transitional Boundary Layers in Incompressible Flows. Springer, Berlin, Heidelberg, New York, 1999.

    Google Scholar 

  • N. A. Cumpsty. Compressor Aerodynamics. Longman Scientific & Technical, Harlow, 1989.

    Google Scholar 

  • N. A. Cumpsty. Jet Propulsion. Cambridge University Press, Cambridge, 1997.

    Google Scholar 

  • J. D. Denton. An Improved Time Marching Method for Turbomachinery Flow Calculation. 82-GT-239, ASME, Int. Gas Turbine Conf., Wembley, 1987.

    Google Scholar 

  • S. L. Dixon. Fluid Mechanics, Thermodynamics of Turbomachinery. Pergamon Press, Oxford, 1975.

    Google Scholar 

  • J. H. Ferziger, M. Peric. Computational Methods for Fluid Dynamics. Springer, Berlin, Heidelberg, New York, 2002.

    Google Scholar 

  • S. J. Galimore, N. A. Cumpsty. Spanwise Mixing in Axial Flow Turbomachines. Transactions of the ASME, Journal of Turbomachinery, 108, 10–16, 1986.

    Google Scholar 

  • J. P. Gostelow. Cascade Aerodynamics. Pergamon Press, Oxford, 1984.

    Google Scholar 

  • P. G. Hill, C. R. Peterson. Mechanics and Thermodynamics of Propulsion. Addison-Wesley Publishing Company, Reading, Mass., 1992.

    Google Scholar 

  • J. H. Horlock. Axial Flow Compressors: Fluid Mechanics and Thermodynamics. Butterworth, London, 1958.

    Google Scholar 

  • K. Jacob, F. W. Riegels. The Calculation of the Pressure Distribution over Aerofoil Sections of Finite Thickness with and without Flaps and Slats. Zeitschrift f. Flugwissenschaft, 11,9, 357–367, 1963.

    Google Scholar 

  • J. K. Kerrebrock. Aircraft Engines and Gas Turbines. MIT Press, Cambridge, Mass., 1996.

    Google Scholar 

  • S. Lieblein. Experimental Flow in Two-Dimensional Cascades. Research Memorandum, RM E56B03, NACA, 1956.

    Google Scholar 

  • S. Lieblein. Loss and Stall Analysis of Compressor Cascade. Transactions of the ASME, J. of Basic Engineering, 81, 387, 1959.

    Google Scholar 

  • S. Lieblein. Incidence and Deviation-Angle Correlations for Compressor Cascades. Transactions of the ASME, J. of Basic Engineering, 82, 575–587, 1960.

    Google Scholar 

  • S. Lieblein, F. C. Schwenk, R. L. Broderick. Diffusion Factor for Estimated Losses and Limiting Blade Loadings in Axial Compressor Blade Elements. Research Memorandum, RM E53D01, NACA, 1953.

    Google Scholar 

  • E. Martensen. Berechnung der Druckverteilung an Gitterprofilen in ebener Potentialströmung mit einer Fredholmschen Integralgleichung. Archive for Rational Mechanic and Analysis, 3, 235–270, 1959.

    MATH  MathSciNet  Google Scholar 

  • J. D. Mattingly. Elements of Gas Turbine Propulsion. McGraw-Hill, New York, 1996.

    Google Scholar 

  • H. Oertel Jr., E. Laurien. Numerische Strömungsmechanik. Vieweg, Wiesbaden, Braunschweig, 2003.

    Google Scholar 

  • S. V. Patankar. Numerical Heat Transfer and Fluid Flow. Taylor & Francis, Bristol, PA, 1980.

    Google Scholar 

  • L. H. Smith. The Radial Equilibrium Equation of Turbomachinery. Transactions of the ASME, Journal of Engineering for Power, 88,1, 1–12, 1966.

    Google Scholar 

  • S. F. Smith. A Simple Correlation of Turbine Efficiency. J. of the Royal Aeronautical Society, 69, 467, 1965.

    Google Scholar 

  • J. D. Stanitz. Some Theoretical Aerodynamical Investigations of Impellers in Radial and Mixed-Flow-Centrifugal Compressors. Transactions of the ASME, 74, 4, 1952.

    Google Scholar 

  • J. D. Stanitz, G. O. Ellis. Two-Dimensional Compressible Flow in Centrifugal Compressors with Straight Blades. Report 954, NACA, 1952.

    Google Scholar 

  • A. Stodola. Steam and Gas Turbines, with a Supplement on the Prospects of the Thermal Prime Mover. McGraw-Hill, New York, 1927.

    Google Scholar 

  • B. S. Stratford. The Prediction of Separation of the Turbulent Boundary Layer. JFM, 5, 1–16, 1959.

    MATH  MathSciNet  Google Scholar 

  • J. C. Tannehill, D. A. Anderson, R. H. Pletcher. Computational Fluid Mechanics and Heat Transfer. Taylor & Francis, Washington, DC, 1997.

    Google Scholar 

  • D. L. Tipton. Improved techniques for compressor loss calculations. T. F. Nagey, ed., Advanced Components for Turbojet Engines, CP-34, 7/1-7/23, Neuilly-sur-Seine, 1968. AGARD.

    Google Scholar 

  • W. Traupel. Calculation of Potential Flow Through Grids. 1, Sluzer Technical Review, 1945.

    Google Scholar 

  • P. P. Walsh, P. Fletcher. Gas Turbine Performance. Blackwell Science Inc., Oxford, 1998.

    Google Scholar 

  • A. J. Wennertrom. Design of Highly Loaded Axial-Flow Fans and Compressors. Concepts ETI Inc., White River Junction, VT, 2000.

    Google Scholar 

  • D. H. Wilkinson. A Numerical Solution of the Analysis and Design Problems for the Flow Past One or More Aerofoils or Cascades. Report 3545, Aeronautical Research Council., London, 1968.

    Google Scholar 

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(2004). Thermal Turbomachinery. In: Oertel, H. (eds) Prandtl’s Essentials of Fluid Mechanics. Applied Mathematical Sciences, vol 158. Springer, New York, NY. https://doi.org/10.1007/0-387-21803-3_14

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  • DOI: https://doi.org/10.1007/0-387-21803-3_14

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-0-387-40437-0

  • Online ISBN: 978-0-387-21803-8

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