1-24 of 42 Books
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
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
Electro-mechanical actuator
Electro-mechanical actuator
By Kenneth E. Schreiner
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
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
High-Alpha Research Vehicle (HARV) longitudinal controller
High-Alpha Research Vehicle (HARV) longitudinal controller
By Aaron J. Ostroff
Flight testing the X-36--the test pilot's perspective
Flight testing the X-36--the test pilot's perspective
By Laurence A. Walker
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
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
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
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
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
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
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
Integrated control using the SOFFT control structure
Integrated control using the SOFFT control structure
By Nesim Halyo
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
HARV ANSER flight test data retrieval and processing procedures
HARV ANSER flight test data retrieval and processing procedures
By Jessie C. Yeager
The control system for the X-33 linear aerospike engine
The control system for the X-33 linear aerospike engine
By Jerry E. Jackson
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
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
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
A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
By Steven A. Johnson
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
Relative control effectiveness technique with application to airplane control coordination
Relative control effectiveness technique with application to airplane control coordination
By Frederick J. Lallman