C Asbury Scott

发表

A Passive Cavity Concept for Improving the Off-Design Performance of Fixed Geometry Exhaust Nozzles

C Asbury Scott, A Hunter Craig, L Gunther Chistopher, 1996 .

A Static Investigation of the Thrust Vectoring System of the F/A-18 High-Alpha Research Vehicle

C Asbury Scott, L Mason Mary, J Capone Francis, 1992 .

Static Performance of a Wing-Mounted Thrust Reverser Concept

C Asbury Scott, A Yetter Jeffrey, 1998 .

Internal Performance of Highly Integrated Deployable Exhaust Nozzles

C Asbury Scott, L Mason Mary, Lamb Milton, 1995 .

Internal Performance of a Fixed-Shroud Nonaxisymmetric Nozzle Equipped With an Aft-Hood Exhaust Deflector

C Asbury Scott, 1997 .

Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control

C Asbury Scott, A Hunter Craig, 1999 .

Static Performance of Six Innovative Thrust Reverser Concepts for Subsonic Transport Applications - Summary of the NASA Langley Innovative Thrust Reverser Test Program

C Asbury Scott, A Yetter Jeffrey, S. Asbury, 2000 .

An Experimental and Computational Investigation of a Translating Throat Single Expansion-Ramp Nozzle

C Asbury Scott, A Deere Karen, 1996 .

Multiaxis Thrust-Vectoring Characteristics of a Model Representative of the F-18 High-Alpha Research Vehicle at Angles of Attack From 0 to 70

C Asbury Scott, J Capone Francis, 1995 .

Static Performance of a Cruciform Nozzle With Multiaxis Thrust-Vectoring and Reverse-Thrust Capabilities

C Asbury Scott, J Wing David, 1992 .

Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds

C Asbury Scott, R Carlson John, 1994 .