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.
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.
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.
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.
Katsanis, Theodore:
Velocity Gradient Method for Calculating Velocities in an
Axisymmetric Annular Duct.
NASA Technical Paper 2029, July 1982.
Mechtly, E. A.:
The International System of Units, Physical Constants and Conversion Factors.NASA Special Publication 7012, 2nd rev., 1973.
Vavra, Michael H.: Aero-Thermodynamics and Flow in Turbomachines.
Robert E. Krieger Publ. Co., 1974.
Carnahan, Brice; Luther, H. A.; and Wilkes, James O.:
Applied Numerical Methods. John Wiley & Sons, Inc., 1969.
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.
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.
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.
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.
McNally, William D.:
FORTRAN Program for Generating a Two-Dimensional
Orthogonal Mesh Between Two Arbitrary Boundaries.
NASA Technical Note D-6766, April 1972.
McCracken, Daniel D.; and Dorn, William S.:
Numerical Methods and FORTRAN Programming. John Wiley & Sons, Inc., 1964.
Varga, Richard S.: Matrix Iterative Analysis. Prentice-Hall, Inc., 1962.
Shapiro, Ascher H.:
The Dynamics and Thermodynamics of Compressible Fluid Flow. Vol. I.
Ronald Press Co., 1953.
Crouse, James:
Computer Program for the Definition of Transonic Axial-Flow Compressor Blade Rows.
NASA Technical Note D-7345, February 1974.
Johnsen, Irving A.; and Bullock, Robert O., eds.:
Aerodynamic Design of Axial-Flow Compressors.
NASA Special Publication 36, 1965.
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.
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.
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.
Schumann, Lawrence F.:
FORTRAN Program for Calculating Leading- and Trailing-Edge Geometry
of Turbomachine Blades.
NASA Technical Memorandum X-73679, 1977.
Kannenberg, Robert G.:
CINEMATIC - FORTRAN Subprograms for Automatic Computer Microfilm Plotting.
NASA TM X-1866, 1969.