Add to ORKGLow-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-floating canard surface
The present investigation was conducted in the Langley high-speed 7-by 10-foot tunnel to determine t...
An experimental investigation of the low-speed static longitudinal, lateral and directional stabilit...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
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...
An investigation at low subsonic speeds has been conducted in the Langley 300-MPH 7- by 10-foot tunn...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
An experimental wind-tunnel investigation has been carried out to determine the static longitudinal,...
Static longitudinal stability and control characteristics of air-to-surface canard missile configura...
An investigation was made to determine the effects of wing position and fuselage size on the low-spe...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged miss...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
The present investigation was conducted in the Langley high-speed 7-by 10-foot tunnel to determine t...
An experimental investigation of the low-speed static longitudinal, lateral and directional stabilit...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
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...
An investigation at low subsonic speeds has been conducted in the Langley 300-MPH 7- by 10-foot tunn...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
A 0.36-scale model of a canard general-aviation airplane with a single pusher propeller and winglets...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
An experimental wind-tunnel investigation has been carried out to determine the static longitudinal,...
Static longitudinal stability and control characteristics of air-to-surface canard missile configura...
An investigation was made to determine the effects of wing position and fuselage size on the low-spe...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged miss...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
The present investigation was conducted in the Langley high-speed 7-by 10-foot tunnel to determine t...
An experimental investigation of the low-speed static longitudinal, lateral and directional stabilit...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...