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canard wings

1-24 of 36 Books

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 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 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 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 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 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 Basic low speed aerodynamics of the short-coupled canard configuration of small aspect ratio By Hermann Behrbohm

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

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 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 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 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 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 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 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 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 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 A look at handling qualities of canard configurations By Seth B. Anderson

A look at handling qualities of canard configurations

A look at handling qualities of canard configurations

By Seth B. Anderson

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 Parametric study of a canard-configured transport using conceptual design optimization By P. Douglas Arbuckle

Parametric study of a canard-configured transport using conceptual design optimization

Parametric study of a canard-configured transport using conceptual design optimization

By P. Douglas Arbuckle

View The effect of a canard surface on the total lift of an unswept wing in subsonic flow By Maurice Lee Rasmussen

The effect of a canard surface on the total lift of an unswept wing in subsonic flow

The effect of a canard surface on the total lift of an unswept wing in subsonic flow

By Maurice Lee Rasmussen

View Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration By Blair B Gloss

Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration

Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration

By Blair B Gloss

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