Francis J. Capone

• Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
• Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20
• Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings
• Effects of empennage surface location on aerodynamic characteristics of a twin-engine afterbody model with nonaxisymmetric nozzles
• Multiaxis aircraft control power from thrust vectoring at high angles of attack
• Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47
• Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20
• Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability
• The NASA Langley 16-Foot Transonic Tunnel
• The NASA Langley 16-foot transonic tunnel