W.H. Mason and J.F. Marchman III, “Farfield Structure of Aircraft Wake Turbulence,” Journal of Aircraft, Vol. 10, No. 2, February 1973, pp.86-92.
G.R. Inger and W.H. Mason, “Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer Interaction,” AIAA J., Vol. 14, No. 9, September 1976, pp.1266-1272.
W.H. Mason, D.A. MacKenzie, M.A. Stern, W.F Ballhaus Jr., and J. Frick, “Automated Procedure for Computing the Three-Dimensional Transonic Flow Over Wing-Body Combinations, including Viscous Effects,” Vol. I, Description of Methods and Applications (a 5.3M pdf file), Vol. II, Program User's Manual, AFFDL-TR-77-122, February 1978.
W.H. Mason, D.A. MacKenzie, M.A. Stern, and J.K. Johnson, “A Numerical Three Dimensional Viscous Transonic Wing-Body Analysis and Design Tool,” AIAA Paper No. 78-101, January 1978.
W.H. Mason and G. DaForno, “Opportunities for Supersonic Performance Gains Through Non-Linear Aerodynamics,” AIAA Paper No. 79-1527, July 1979.
W.H. Mason and D.S. Miller, “Controlled Supercritical Crossflow on Supersonic Wings - An Experimental Validation,” AIAA Paper No. 80-1421, July 1980.
D.S. Miller, E.J. Landrum, J.C. Townsend, and W.H. Mason, “Pressure and Force Data for a Flat Wing and a Warped Conical Wing Having a Shockless Recompression at Mach 1.62,” NASA TP 1759, April 1981.
W.H. Mason, “Wing-Canard Aerodynamics at Transonic Speeds - Fundamental Considerations on Minimum Drag Spanloads,” AIAA Paper No. 82-0097, January 1982
W.H. Mason, Aerodynamic Calculation Methods for Programmable Calculators and Personal Computers, Aerocal, 1982, Pak#1: “Basic Aerodynamic Relations,” Pak#2: “Basic Geometry for Aerodynamics,” Pak#3: “Basic Subsonic Aerodynamics,” Pak#4: “Boundary Layer Analysis Methods”.
W.H. Mason, D.S. Miller, J.L. Pittman, and M.J. Siclari, “A Supersonic Maneuver Wing Designed for Nonlinear Attached Flow,” AIAA Paper No. 83-0425, January 1983.
W.H. Mason and B.S. Rosen, “The COREL and W12SC3 Computer Programs for Supersonic Wing Design and Analysis,” NASA CR 3676, December 1983.
W.H. Mason, “SC3 - A Wing Concept for Supersonic Maneuvering,” AIAA Paper No. 83-1858, July 1983.
P.V. Aidala, W.H. Davis, Jr., and W.H. Mason, “Smart Aerodynamic Optimization,” AIAA Paper No. 83-1863, July 1983.
W.H. Mason, “A Wing Concept for Supersonic Maneuvering,” NASA CR 3763, Dec. 1983.
M. Siclari, M. Visich, A. Cenko, B. Rosen, and W.H. Mason, “An Evaluation of NCOREL, PAN AIR and W12SC3 for the Prediction of Pressure on a Supersonic Maneuver Wing,” Journal of Aircraft, Vol. 21, No. 10, pp 816-822, Oct. 1984
J.L. Pittman, D.S. Miller, and W.H. Mason, “Fuselage and Canard Effects on an Attached Flow, Maneuver Wing at Mach 1.62,” NASA TP 2249, February 1984
J.L. Pittman, D.S. Miller, and W.H. Mason, “Supersonic, Nonlinear, Attached-Flow Wing Design for High Lift with Experimental Validation,” NASA TP 2336, August 1984.
R.E. Melnik and W.H. Mason, “Mass Flux Boundary Conditions in Linear Theory,” AIAA J., Vol. 22, No. 11, November 1984.
W.H. Davis, Jr., P.V. Aidala, and W.H. Mason, “A Study to Develop Improved Methods for the Design of Transonic Fighter Wings by the Use of Numerical Optimization,” NASA CR 3995, August 1986.