S. Naomi McMillin

• Effect of planform and body on supersonic aerodynamics of multibody configurations
• Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings
• Planform effects on the supersonic aerodynamics of multibody configurations
• Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber