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thrust vector control

1-24 of 42 Books

View Optimal pitch thrust-vector angle and benefits for all flight regimes By Glenn B. Gilyard

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

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

By Glenn B. Gilyard

View Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring By Kenneth W. Iliff

Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring

Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring

By Kenneth W. Iliff

View High-Alpha Research Vehicle (HARV) longitudinal controller By Aaron J. Ostroff

High-Alpha Research Vehicle (HARV) longitudinal controller

High-Alpha Research Vehicle (HARV) longitudinal controller

By Aaron J. Ostroff

View Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle By Scott C. Asbury

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

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

By Scott C. Asbury

View Electro-mechanical actuator By Kenneth E. Schreiner

Electro-mechanical actuator

Electro-mechanical actuator

By Kenneth E. Schreiner

View A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors By Kenneth H. Goodrich

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

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

By Kenneth H. Goodrich

View Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane By David E. Reubush

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

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

By David E. Reubush

View Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes By Robert J. Foley

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

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

By Robert J. Foley

View Flight testing the X-36--the test pilot's perspective By Laurence A. Walker

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

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

By Laurence A. Walker

View Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows By Scott T. Imlay

Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

By Scott T. Imlay

View An experimental/modeling study of jet attachment during counterflow thrust vectoring By Paul J. Strykowski

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

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

By Paul J. Strykowski

View Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability By David J. Wing

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

By David J. Wing

View The control system for the X-33 linear aerospike engine By Jerry E. Jackson

The control system for the X-33 linear aerospike engine

The control system for the X-33 linear aerospike engine

By Jerry E. Jackson

View HARV ANSER flight test data retrieval and processing procedures By Jessie C. Yeager

HARV ANSER flight test data retrieval and processing procedures

HARV ANSER flight test data retrieval and processing procedures

By Jessie C. Yeager

View A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane By Frederick J. Lallman

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane

By Frederick J. Lallman

View An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques By William G. Schweikhard

An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques

An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques

By William G. Schweikhard

View 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

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 70 ̊

By Scott C. Asbury

View Integrated control using the SOFFT control structure By Nesim Halyo

Integrated control using the SOFFT control structure

Integrated control using the SOFFT control structure

By Nesim Halyo

View Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control By Scott C. Asbury

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

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

By Scott C. Asbury

View Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft By Martin J. Brenner

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

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

By Martin J. Brenner

View Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application By Jagdish S. Sokhey

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application

By Jagdish S. Sokhey

View Electromechanical actuation for thrust vector control applications By Mary Ellen Roth

Electromechanical actuation for thrust vector control applications

Electromechanical actuation for thrust vector control applications

By Mary Ellen Roth

View Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle By W. Thomas Bundick

Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle

Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle

By W. Thomas Bundick

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

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

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

By Jing-Biau Tseng