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Last edited by ImportBot
September 14, 2008 | History
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Scott C. Asbury

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9 works Add another?

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

    First published in 1993 4 editions in 1 language
    Not in Library

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

    First published in 1995 2 editions in 1 language
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  • Cover of: Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

    First published in 1999 2 editions in 1 language
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  • Cover of: Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle

    First published in 1999 1 edition in 1 language
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  • Cover of: Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

    First published in 1997 1 edition in 1 language
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  • Cover of: Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft

    First published in 1995 1 edition
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  • Cover of: 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

    First published in 1995 1 edition
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  • Cover of: Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊

    First published in 1995 1 edition in 1 language
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  • Cover of: Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

    First published in 2000 1 edition in 1 language
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We need a photo of Scott C. Asbury

Subjects
Thrust vector control, Nozzles, F-18 aircraft, Exhaust nozzles, Research vehicles, Wind tunnel tests, Aeronautical engineering, Aircraft brakes, Aircraft design, Boundary layer separation, Brakes (For arresting motion), Cavities, Convergent-divergent nozzles, Deflectors, Flow visualization, Hole geometry (Mechanics), Jet nozzles, Nozzle flow, Oblique shock waves, Performance tests, Porosity, Short takeoff aircraft, Subsonic speed, Thrust reversal, Turbofans

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ID Numbers

  • OLID: OL4666816A

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History

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September 14, 2008 Created by ImportBot Imported from Oregon Libraries MARC record