1-24 of 36 Books
Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing
Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing
By Thomas G. Gainer
High-angle-of-attack stability characteristics of a three-surface fighter configuration
High-angle-of-attack stability characteristics of a three-surface fighter configuration
By Sue Grafton
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
By Dale R. Satran
Wind-tunnel investigation of an advanced general aviation canard configuration
Wind-tunnel investigation of an advanced general aviation canard configuration
By Joseph R. Chambers
A study of canard-wing interference using experimental pressure data at transonic speeds
A study of canard-wing interference using experimental pressure data at transonic speeds
By Blair B. Gloss
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
By A. B. Blair
An in-flight interaction of the X-29A canard and flight control system
An in-flight interaction of the X-29A canard and flight control system
By M. W. Kehoe
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization
By Harry W. Carlson
Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards
Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards
By Mary L. Mason
A study of canard-wing interference using experimental pressure data at transonic speeds
A study of canard-wing interference using experimental pressure data at transonic speeds
By Blair B Gloss
High angle canard missile test in the Ames 11-foot transonic wind tunnel
High angle canard missile test in the Ames 11-foot transonic wind tunnel
By Richard G. Schwind
Basic low speed aerodynamics of the short-coupled canard configuration of small aspect ratio
Basic low speed aerodynamics of the short-coupled canard configuration of small aspect ratio
By Hermann Behrbohm
High-angle-of-attack stability characteristics of a three-surface fighter configuration
High-angle-of-attack stability characteristics of a three-surface fighter configuration
By Sue Grafton
Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20
Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20
By Richard J. Re
Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center
Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center
By Richmond P. Boyden
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
By A. B Blair
Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing
Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing
By Gainer, Thomas G
Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds
Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds
By Blair B. Gloss
Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen
Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen
By A. Bergmann
Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
By Francis J Capone
Body and canard effects on an attached-flow maneuver wing at Mach 1.62
Body and canard effects on an attached-flow maneuver wing at Mach 1.62
By Jimmy L Pittman
Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center
Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center
By Richmond P Boyden
Effect of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration
Effect of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration
By Long P Yip