Francis J Capone

• Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
• Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft
• Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
• Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model
• Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
• Statis performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability