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  1. Katsanis, Theodore: Use of Arbitrary Quasi-Orthogonals for Calculating Flow Distribution in the Meridional Plane of a Turbomachine. NASA Technical Note D-2546, December 1964.
  2. Katsanis, Theodore: A Computer Program for Calculating Velocities and Streamlines for Two-Dimensional, Incompressible Flow In Axial Blade Rows. NASA Technical Note D-3762, January 1967.
  3. Katsanis, Theodore; and McNally, William D.: Revised Fortran Program for Calculating Velocities and Streamlines on the Hub-Shroud Midchannel Stream Surface of an Axial-, Radial-, or Mixed-Flow Turbomachine or Annular Duct, Vol. I - User's Manual. NASA Technical Note D-8430, March 1977.
  4. Katsanis, Theodore; and McNally, William D.: Revised Fortran Program for Calculating Velocities and Streamlines on the Hub-Shroud Midchannel Stream Surface of an Axial-, Radial-, or Mixed-Flow Turbomachine or Annular Duct, Vol. II - Programmer's Manual. NASA Technical Note D-8431, July 1977.
  5. Katsanis, Theodore: Velocity Gradient Method for Calculating Velocities in an Axisymmetric Annular Duct. NASA Technical Paper 2029, July 1982.
  6. Mechtly, E. A.: The International System of Units, Physical Constants and Conversion Factors. NASA Special Publication 7012, 2nd rev., 1973.
  7. Vavra, Michael H.: Aero-Thermodynamics and Flow in Turbomachines. Robert E. Krieger Publ. Co., 1974.
  8. Carnahan, Brice; Luther, H. A.; and Wilkes, James O.: Applied Numerical Methods. John Wiley & Sons, Inc., 1969.
  9. Wu, Chung-Hua: A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial-, Radial-, and Mixed-Flow Types. NACA Technical Note 2604, January 1952.
  10. Katsanis, Theodore: FORTRAN Program for Calculating Transonic Velocities on a Blade-to-Blade Stream Surface of a Turbomachine. NASA Technical Note D-5427, September 1969.
  11. Katsanis, Theodore; and McNally, William D.: FORTRAN Program for Calculating Velocities and Streamlines on the Hub-Shroud Mid-Channel Flow Surface of an Axial- or Mixed-Flow Turbomachine. I - User's Manual. NASA Technical Note D-7343, July 1973.
  12. Katsanis, Theodore; and McNally, William D.: FORTRAN Program for Calculating Velocities and Streamlines on the Hub-Shroud Mid-Channel Flow Surface of an Axial- or Mixed-Flow Turbomachine. II - Programmer's Manual. NASA Technical Note D-7344, April 1974.
  13. McNally, William D.: FORTRAN Program for Generating a Two-Dimensional Orthogonal Mesh Between Two Arbitrary Boundaries. NASA Technical Note D-6766, April 1972.
  14. McCracken, Daniel D.; and Dorn, William S.: Numerical Methods and FORTRAN Programming. John Wiley & Sons, Inc., 1964.
  15. Varga, Richard S.: Matrix Iterative Analysis. Prentice-Hall, Inc., 1962.
  16. Shapiro, Ascher H.: The Dynamics and Thermodynamics of Compressible Fluid Flow. Vol. I. Ronald Press Co., 1953.
  17. Crouse, James: Computer Program for the Definition of Transonic Axial-Flow Compressor Blade Rows. NASA Technical Note D-7345, February 1974.
  18. Johnsen, Irving A.; and Bullock, Robert O., eds.: Aerodynamic Design of Axial-Flow Compressors. NASA Special Publication 36, 1965.
  19. Katsanis, Theodore: FORTRAN Program for Quasi-Three-Dimensional Calculation of Surface Velocities and Choking Flow for Turbomachine Blade Rows. NASA Technical Note D-6177, April 1971.
  20. Walsh, J. L.: Ahlberg, J. H.; and Nilson, E. N.: Best Approximation Properties of the Spline Fit. J. Math. Mech., vol. 11, no. 2, 1962, pp. 225-234.
  21. Stanitz, John D. and Prian, Vasily D.: A Rapid Approximate Method for Determining Velocity Distribution on Impeller Blades of Centrifugal Compressors. NACA Technical Note 2421, July 1951.
  22. Schumann, Lawrence F.: FORTRAN Program for Calculating Leading- and Trailing-Edge Geometry of Turbomachine Blades. NASA Technical Memorandum X-73679, 1977.
  23. Kannenberg, Robert G.: CINEMATIC - FORTRAN Subprograms for Automatic Computer Microfilm Plotting. NASA TM X-1866, 1969.
PDAS home > Contents > Annular Duct > References
Public Domain Aeronautical Software (PDAS)