Thrust Vector Control

53 books
Electromechanical actuation for thrust vector control applicationsMary Ellen Roth

Electromechanical actuation for thrust vector control applications

Mary Ellen Roth

1990No page data
Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzleScott C. Asbury
⏱ 1h 47m

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

Scott C. Asbury

1993107 pp.
A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectorsKenneth H. Goodrich
⏱ 24m

A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors

Kenneth H. Goodrich

198924 pp.
Flight testing the X-36--the test pilot's perspectiveLaurence A. Walker

Flight testing the X-36--the test pilot's perspective

Laurence A. Walker

1997No page data
Optimal pitch thrust-vector angle and benefits for all flight regimesGlenn B. Gilyard
⏱ 22m

Optimal pitch thrust-vector angle and benefits for all flight regimes

Glenn B. Gilyard

200022 pp.
Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversersRobert S. Green
⏱ 40m

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

Robert S. Green

198740 pp.
A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicleMary L. Mason
⏱ 2h 42m

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle

Mary L. Mason

1992162 pp.
Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplaneDavid E. Reubush
⏱ 1h 57m

Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane

David E. Reubush

1987117 pp.
High-Alpha Research Vehicle (HARV) longitudinal controllerAaron J. Ostroff

High-Alpha Research Vehicle (HARV) longitudinal controller

Aaron J. Ostroff

1994No page data
TVC jet vane thermal modeling using parametric system identificationR. H. Nunn
⏱ 1h 0m

TVC jet vane thermal modeling using parametric system identification

R. H. Nunn

198860 pp.
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 degScott C. Asbury
⏱ 2h 53m

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

Scott C. Asbury

1995173 pp.
Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"Jing-Biau Tseng

Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"

Jing-Biau Tseng

1989No page data
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊Scott C. Asbury

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

Scott C. Asbury

1995No page data
Evaluation of four advanced nozzle concepts for short takeoff and landing performanceP. Frank Quinto
⏱ 1h 35m

Evaluation of four advanced nozzle concepts for short takeoff and landing performance

P. Frank Quinto

199395 pp.
An experimental/modeling study of jet attachment during counterflow thrust vectoringPaul J. Strykowski

An experimental/modeling study of jet attachment during counterflow thrust vectoring

Paul J. Strykowski

1997No page data
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction controlScott C. Asbury

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

Scott C. Asbury

1999No page data
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanesRobert J. Foley
⏱ 1h 17m

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Robert J. Foley

199177 pp.
HARV ANSER flight test data retrieval and processing proceduresJessie C. Yeager

HARV ANSER flight test data retrieval and processing procedures

Jessie C. Yeager

1997No page data
Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplaneUnknown Author

Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane

Unknown Author

1996No page data
Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraftMartin J. Brenner

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft

Martin J. Brenner

1996No page data
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