Richard J Re

• An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90
• Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20
• Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles
• Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing