The first reference is the primary reference for this program.
Mason, William H.; and Rosen, Bruce S.:
The COREL and W12SC3 Computer
Programs for Supersonic Wing Design and Analysis.
NASA Contractor Report 3676, 1983.
Miller, D.S.; Carlson, H.W.; and Middleton, W.D.:
A Linearized Theory Method of Constrained Optimization for Supersonic Cruise Wing Design.
Proc. of the SCAR Conf., NASA Conference Publication CP-001, November 1976.
Mason, W.H.; and Miller, D.S.:
Controlled Supercritical Crossflow on Supersonic Wings - An Experimental Validation.
AIAA Paper No. 80-1421, July, 1980.
Mason, W.H.; and DaForno, G.:
Opportunities for Supersonic Performance Gains Through Non-Linear Aerodynamics.
AIAA Paper No. 79-1527, July 1979.
Grossman, B.,
A Numerical Procedure for the Computation of Supersonic Conical Flows.
AIAA Journal, Vol. 17, No. 8, Aug. 1979, pp. 828-837.
Woodward, F.A.:
An Improved Method for the Aerodynamic Analysis of
Wing-Body-Tail Configurations in Subsonic and Supersonic Flow.
NASA Contractor Report 2228, Parts I and II, 1973.
Craidon, C.B.:
A Computer Program for Fitting Smooth Surfaces to an
Aircraft Configuration and Other Three-Dimensional Geometries.
NASA Technical Memorandum X-3206, June 1975.
Siclari, M.J.; and Marconi F.:
Analysis and Design of Supersonic Aircraft Based on Inviscid Nonlinear
Eulerian Equations, Part I, Rotational Euler Solutions with Explicit Shock Fitting.
AFWAL TR-80-3110, October 1980, pp. 53-56.
Woodward, F.A.:
USSAERO Computer Program Development, Versions B and C.
NASA Contractor Report 3227, April 1980.
Woodward, F.A.; Tinoco, E.N.; and Larsen, J.W.:
Analysis and Design of Supersonic Wing-Body Combinations,
Including Flow Properties in the Near Field, Part I - Theory and Application.
NASA Contractor Report 73106, August 1967.
Cenko, A.: Advances in Supersonic Configuration Design Methods.
Journal of Aircraft, Vol. 17, No. 2, Feb. 1980, pp. 119-126.
Carlson, H.W.:
A Modification to Linearized Theory for Prediction of
Pressure Loadings on Lifting Surfaces at High Supersonic Mach Numbers and
Large Angles of Attack.
NASA Technical Publication 1406, February 1979.
Craidon, C.B.:
Description of a Digital Computer Program for Airplane Configuration Plots.
NASA Technical Memorandum X-2074, September 1970.
Miller, D.S.; Landrum, E.J.; Townsend, J.C.; and Mason, W.H.:
Pressure and Force Data for a Flat Wing and a Warped Conical Wing Having a Shockless
Recompression at Mach 1.62.
NASA Technical Publication 1759, April 1981.
Siclari, M.J.; and Grossman, B.:
Analysis and Design of Supersonic Aircraft
Based on Inviscid Nonlinear Eulerian Equations, Part II, Nonlinear Potential
Flow Solutions with Shock Capturing.
AFWAL TR-80-3110, October 1980.
Mason, W.H.:
Experimental Pressure Distributions and Aerodynamic Characteristics
of a Demonstration Wing for a Wing Concept for Supersonic Maneuvering.
Grumman Aerodynamics Report 393-82-02, July 1982.
Grossman, B.; and Siclari, M.J.:
The Nonlinear Supersonic Potential Flow over Delta Wings.
AIAA Paper No. 80-0269, January 1980.
Mason, W.H.:
Experimental Pressure Distributions and Aerodynamic Characteristics
of Flat and Cambered Conceptual Wing-Body and Wing-Body-Canard.
Grumman Aerodynamics Report 393-81-1, October 1981.