Explore Books on
fighter aircraft
1-24 of 49 Books
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By Donald R. Riley
Lateral-directional eigenvector flying qualities guidelines for high performance aircraft
Lateral-directional eigenvector flying qualities guidelines for high performance aircraft
By John B. Davidson
Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
By John E. Lamar
Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing
Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing
By John W. Smith,Wilton P. Lock
Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft
Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft
By Murphy, Patrick C.
Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
By Jay M. Brandon
Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
By Dale R. Satran
Wind-tunnel free-flight investigation of a supersonic persistence fighter
Wind-tunnel free-flight investigation of a supersonic persistence fighter
By David E. Hahne
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
The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft
The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft
By Bradford Neal
Robust, decoupled, flight control design with rate saturated actuators
Robust, decoupled, flight control design with rate saturated actuators
By S. A. Snell
Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions
Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions
By James C. Ferris
Performance study for inlet installations
Performance study for inlet installations
By D. C. Bingaman
Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
By Scott P. Fears
Aerodynamics of combat aircraft controls and of ground effects
Aerodynamics of combat aircraft controls and of ground effects
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Special course on fundamentals of fighter aircraft design
Special course on fundamentals of fighter aircraft design
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Vortex flow aerodynamics
Vortex flow aerodynamics
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
By Vladislav Klein
Jaguar
Jaguar
By Roger Chesneau,Ray Rimell,Raymond L. Rimell
Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
By James A. Franklin
Improvement to the adaptive maneuvering logic program
Improvement to the adaptive maneuvering logic program
By George H. Burgin
Euler technology assessment for preliminary aircraft design
Euler technology assessment for preliminary aircraft design
By Todd R. Michal
Standardized environmental fatigue sequence for the evaluation of composite components in combat aircraft (ENSTAFF = ENvironmental FalSTAFF)
Standardized environmental fatigue sequence for the evaluation of composite components in combat aircraft (ENSTAFF = ENvironmental FalSTAFF)
By J. J. Gerharz