Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane / James L. Dillon and Jimmy L. Pittman, Langley Research Center.James L. Dillon1978
Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of Wing-body Design Concept for a Hypersonic Research Airplane / James L. Dillon and Jimmy L. Pittman.James L. Dillon1977
Aerodynamic Characteristics of a Hypersonic Cruise Aircraft Concept with Wing-mounted Propulsion Systems at Mach Numbers of 2.96, 3.96, and 4.63 / Gregory D. Riebe and Jimmy L. Pittman.Gregory D. Riebe1981