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wings canard

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View 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

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

View High-angle-of-attack stability characteristics of a three-surface fighter configuration By Sue Grafton

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

View Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration By Dale R. Satran

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

View A study of canard-wing interference using experimental pressure data at transonic speeds By Blair B. Gloss

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

View Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers By A. B. Blair

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

View An in-flight interaction of the X-29A canard and flight control system By M. W. Kehoe

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

View 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

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

View Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards By Mary L. Mason

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

View A study of canard-wing interference using experimental pressure data at transonic speeds By Blair B Gloss

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

View High angle canard missile test in the Ames 11-foot transonic wind tunnel By Richard G. Schwind

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

View High-angle-of-attack stability characteristics of a three-surface fighter configuration By Sue Grafton

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

View 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

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

View Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center By Richmond P. Boyden

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

View Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers By A. B Blair

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

View 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

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

View Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds By Blair B. Gloss

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

View Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen By A. Bergmann

Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen

Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen

By A. Bergmann

View Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft By Francis J Capone

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

View Body and canard effects on an attached-flow maneuver wing at Mach 1.62 By Jimmy L Pittman

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

View Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center By Richmond P Boyden

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

View Effect of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration By Long P Yip

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

View Wind-tunnel investigation of an advanced general aviation canard configuration By Joseph R Chambers

Wind-tunnel investigation of an advanced general aviation canard configuration

Wind-tunnel investigation of an advanced general aviation canard configuration

By Joseph R Chambers

View Approximate neutral point of a subsonic canard aircraft By James D Phillips

Approximate neutral point of a subsonic canard aircraft

Approximate neutral point of a subsonic canard aircraft

By James D Phillips

View Wind-tunnel investigation of an advanced general aviation canard configuration By Joseph R Chambers

Wind-tunnel investigation of an advanced general aviation canard configuration

Wind-tunnel investigation of an advanced general aviation canard configuration

By Joseph R Chambers