Richard J. Re

• A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
• Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration
• Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports
• Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
• Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20
• Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
• Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft
• Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92