Scott C. Asbury

• Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
• Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
• Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector
• Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft
• Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg
• Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
• Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊
• Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
• Static performance of six innovative thrust reverser concepts for subsonic transport applications