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Scott C. Asbury

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Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

by Scott C. Asbury First published in 1993 — 4 editions

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Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

by Scott C. Asbury First published in 1999 — 2 editions

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Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊

by Scott C. Asbury First published in 1995 — 2 editions

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Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle

by Scott C. Asbury First published in 1999 — 1 edition

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Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

by Scott C. Asbury First published in 1997 — 1 edition

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Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊

by Scott C. Asbury First published in 1995 — 1 edition

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Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft

by Scott C. Asbury First published in 1995 — 1 edition

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Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

by Scott C. Asbury First published in 2000 — 1 edition

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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

by Scott C. Asbury First published in 1995 — 1 edition

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OLID: OL4666816A

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