Add to ORKGAn investigation has been made in the Langley spin tunnel to determine the spin and spin-recovery characteristics of the F-111A airplane in the symmetric and asymmetric stores loading conditions. Tests were also made with the model in the clean condition to determine whether the spin-recovery characteristics could be improved by the use of supplementary devices
In accordance with a request of the Bureau of Aeronautics, Navy Department, tests were performed in ...
A supplementary investigation to determine the effect of external fuel tanks on the spin and recover...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale ...
An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin a...
An investigation has been made of a 1/28-scale model of the Grumman A-6A airplane in the Langley spi...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the Grumman AF-2S...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
Spin tests have been performed in the Langley 20-foot free-spinning tunnel on a 1/18-scale model of ...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the McDonnell XP-...
An investigation has been conducted in the Langley spin tunnel to determine the spin and recovery ch...
A spin-tunnel investigation of the spin and recovery characteristics of a 1/25-scale model to the Ge...
An investigation of the spin and recovery characteristics of a scale model of the Grumman XF9F-2 air...
A spin-recovery investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 20...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/24-scale ...
An investigation of the spin and recovery characteristics of a 0.057-scale model of the Chance Vough...
In accordance with a request of the Bureau of Aeronautics, Navy Department, tests were performed in ...
A supplementary investigation to determine the effect of external fuel tanks on the spin and recover...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale ...
An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin a...
An investigation has been made of a 1/28-scale model of the Grumman A-6A airplane in the Langley spi...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the Grumman AF-2S...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
Spin tests have been performed in the Langley 20-foot free-spinning tunnel on a 1/18-scale model of ...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the McDonnell XP-...
An investigation has been conducted in the Langley spin tunnel to determine the spin and recovery ch...
A spin-tunnel investigation of the spin and recovery characteristics of a 1/25-scale model to the Ge...
An investigation of the spin and recovery characteristics of a scale model of the Grumman XF9F-2 air...
A spin-recovery investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 20...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/24-scale ...
An investigation of the spin and recovery characteristics of a 0.057-scale model of the Chance Vough...
In accordance with a request of the Bureau of Aeronautics, Navy Department, tests were performed in ...
A supplementary investigation to determine the effect of external fuel tanks on the spin and recover...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale ...