Discover Canard Wings

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards

Approximate neutral point of a subsonic canard aircraft

Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20

Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft

High-angle-of-attack stability characteristics of a three-surface fighter configuration

Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds

A study of canard-wing interference using experimental pressure data at transonic speeds

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

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50p0s to 74p0s delta wings on common fuselage

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

Wind-tunnel investigation of an advanced general aviation canard configuration

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

High-angle-of-attack stability characteristics of a three-surface fighter configuration

An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90

A look at handling qualities of canard configurations

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

Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

Body and canard effects on an attached-flow maneuver wing at Mach 1.62

Canard, a revolution in flight

A study of canard-wing interference using experimental pressure data at transonic speeds

Wind-tunnel investigation of an advanced general aviation canard configuration

Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration