Add to ORKGLow-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small canard surfaces on directional stabilit
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
An experimental investigation was made in the Langley stability tunnel to determine whether the low-...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
An advanced fighter configuration with a forward-swept wing of aspect ratio 3.28 is tested in the La...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
An investigation was conducted in the Langley 30- by 60-Foot Tunnel to determine the aerodynamic cha...
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determ...
An investigation at low subsonic speeds has been conducted in the Langley 300-MPH 7- by 10-foot tunn...
Wind-tunnel tests of a model of an advanced canard configuration designed for general aviation were ...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
An experimental investigation was made in the Langley stability tunnel to determine whether the low-...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
An advanced fighter configuration with a forward-swept wing of aspect ratio 3.28 is tested in the La...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
An investigation was conducted in the Langley 30- by 60-Foot Tunnel to determine the aerodynamic cha...
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determ...
An investigation at low subsonic speeds has been conducted in the Langley 300-MPH 7- by 10-foot tunn...
Wind-tunnel tests of a model of an advanced canard configuration designed for general aviation were ...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
A wind tunnel investigation was conducted to study the low speed, high angle of attack stability cha...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
An experimental investigation was made in the Langley stability tunnel to determine whether the low-...