The first item is the primary reference for this program and Appendix H of
this document is the users guide for creating an input file..
Cunningham, Atlee M.:
A Steady and Oscillatory Kernel Function Method for Interfering Surfaces
in Subsonic, Transonic and Supersonic Flow.
NASA Contractor Report 144895, September 1976.
Watkins, Charles E.; Woolston, Donald S.; and Cunningham, Herbert J.:
A Systematic Kernel Function Procedure for Determining Aerodynamic Forces on
Oscillatory or Steady Finite Wings at Subsonic Speeds.
NASA Technical Report R-48, June 1959.
Cunningham, Herbert J.:
Application of a Supersonic Kernel Function Procedure to Flutter
Analysis of Thin Lifting Surfaces.
NASA Technical Note D-6012, November 1970.
Cunningham, Herbert J.:
Computer Program for Supersonic Analysis of Thin Lifting Surfaces.
NASA Technical Memorandum X-2913, April 1974.
???, J. Aircraft Nov 1974, p.197
Cunningham, Herbert J.; and Desmaris, Robert N.:
Generalization of the Subsonic Kernel Function in the s-Plane,
with Applications to Flutter Analysis.
NASA Technical Paper 2292, March 1984.
Stenton, T.E.; and Andrew, L.V.:
Transonic Unsteady Aerodynamics for Planar Wings with Trailing Edge
Control Surfaces.
AFFDL-TR-57-180, U.S. Air Force, Aug. 1968.
Magnus, R.; and Yoshihara, H.:
Inviscid Transonic Flow Over Airfoils.
AIAA Journal, vol. 8, no. 12, Dec. 1970, pp. 2157-2162.
Murman, E.; and Cole, J.:
Calculation of Transonic Flows.
AIAA Journal, vol. 9, no. 1, Jan. 1971, pp. 121-141.
Bailey, F.R.; and Steger, J.L.:
Relaxation Techniques for Three-Dimensional Transonic Flow About Wings.
AIAA Paper No. 72-189, Jan. 1972.
Magnus, R.; and Yoshihara, H.:
Finite Difference Calculations of the NACA 64A-410 Airfoil Oscillating
Sinusoidally in Pitch at Mach 0.72.
CASD-NSC-74-004, Office of Naval Research, Aug. 1974.
Cunningham, A.M., Jr.:
The Application of General Aerodynamic Lifting Surface Elements to
Problems in Unsteady Transonic Flow.
NASA Contractor Report 112264, Feb. 1973.
Cunningham, A.M., Jr.:
A Collocation Method for Predicting Oscillatory Subsonic Pressure
Distributions on Interfering Parallel Lifting Surfaces.
AIAA Paper No. 71-329, Apr. 1971.
Cohen, D.:
Formulas for the Supersonic Loading, Lift and Drag of Flat
Swept-Back Wings with Leading Edges Behind the Mach Lines.
NACA Report 1050, 1951.
Ii, J.M.; Borland, C.J.; and Hogley, J.R.:
Prediction of Unsteady Aerodynamic Loadings of Non-Planar Wings and
Wing-Tail Configurations in Supersonic Flow, Part 1 -
Theoretical Development, Program Usage and Application.
AFFDL-TDR-71-108, U.S. Air Force, March 1972.
Woodward, F.A.; and Hague, D.S.:
A Computer Program for the Aerodynamic Analysis and Design
of Wing-Body-Tail Combinations at Subsonic and Supersonic Speeds,
Volume I: Theory and Program Utilization.
ERR-FW-867, Fort Worth Division of General Dynamics, Feb. 1969.
Landrum, E.J.:
A Tabulation of Wind-Tunnel Pressure Data and Section Aerodynamic
Characteristics at Mach Numbers 1.61 and 2.01 for Two Trapezoidal Wings
and Three Delta Wings Having Different Surface Shapes.
NASA Technical Note D-1344, Sept. 1962.
[NOTE: This paper seems to have been withdrawn from the NASA report file. Aug. 2010]
Landahl, M.T.:
Unsteady Transonic Flow.
Pergamon Press, New York, Oxford, London, Paris, 1961.
Lessing, Henry C.; Troutman, John L.; and Menees, Gene P.:
Experimental Determination of the Pressure Distribution
on a Rectangular Wing Oscillating in the First Bending
Mode for Mach Numbers from 0.24 to 1.30.
NASA Technical Note D-344, Dec. 1960.
Becker, J.:
Vergleich gemessener and berechneter instationärer Druckverteilungen
für den hohen Unterschall an einem elastischen gepfeilten Flugel.
EWR-Report Nr. 403-69, Messerschmitt-Bölkow-Blohm, Sept. 1969.
Tijdeman, H.: Correspondence to S. R. Bland on Corrections
to Experimental Data published by NLR, (Amsterdam).
Sept. 1973.
Bergh, H.; Tidjeman, H.; and Zwaan, R.J.: High Subsonic
and Transonic Effects on Pressure Distributions Measured
for a Swept Wing with Oscillating Control Surfaces.
Z. Flugwiss., 18 (1970), Heft 9/10, pp. 339-347 (in English).
Laschka, B.; and Schmid, H.:
Unsteady Aerodynamic Forces on Coplanar Lifting Surfaces in Subsonic Flow
(Wing-Horizontal Tail Interference).
Jahrbuch 1967 der WGLR, pp. 211-222 (in English).
Multhopp, H.:
Methods for Calculating the Lift Distribution of Wings,
(Appendix I, Contributed by W. Mangler).
Report No. Aero-2353, Royal Aircraft Establishment,
Farnborough, Hants, Jan. 1950.
Superceded by R & M 2884, 1955.
Pai, S.:
Introduction to the Theory of Compressible Flow.
D. Van Nostrand Company, Inc., Princeton, Toronto, New York, London, 1959.
Anon.: Tables of Chebyshev Polynomials Sn(x) and Cn(x),
(Introduction by Cornelius Lanczos). Applied Mathematics
Series, 9, National Bureau of Standards, 1952.
Harder, R.L.; and Desmarias, R.N.: Interpolation Using Surface Splines.
Journal of Aircraft, Vol. 9, No. 2, Feb. 1972, pp. 189-191.
Note that there are two distinct researchers named Cunningham working
in this field. This program is from the 1976 report by Atlee Cunningham.