Add to ORKGEffect of vertical tails on low speed static stability characteristics of canard-bomber configuration with very thin wing and slender elliptical fuselag
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected...
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determ...
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
Longitudinal aerodynamic characteristics of 1/30 scale nuclear powered canard aircraft model having ...
The effects were studied of various vertical-tail configurations on the longitudinal and lateral dir...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft mode
Hypersonic aerodynamic characteristics of aircraft configurations with canard control
The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabi...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected...
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determ...
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
Longitudinal aerodynamic characteristics of 1/30 scale nuclear powered canard aircraft model having ...
The effects were studied of various vertical-tail configurations on the longitudinal and lateral dir...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft mode
Hypersonic aerodynamic characteristics of aircraft configurations with canard control
The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabi...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected...
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determ...