An investigation has been conducted in the Langley 20-foot free- spinning tunnel scale model of the Cornelius XFG-1 glider, a tailless design having its wings swept forward 15 degrees. It was previously found to possess erratic spin and recovery characteristics, and tests were made to determine modifications which would lead to normal steady spins with consistently good recoveries. The results of the investigation indicated that modifications that aid not appreciably alter the basic design aid not appreciably improve the spin and recovery characteristics. In this instance it appears that the sweptforward wing is the cause of unsatisfactory spin and recovery characteristics
This paper presents the results of a spin-tunnel investigation of a low-wing model typical of presen...
A supplementary investigation has been conducted in the Langley 20-foot free-spinning tunnel of a l/...
An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin a...
An investigation has been conducted in the Langley 20-foot free- spinning tunnel scale model of the ...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
Spin tests have been conducted in the Langley free-spinning tunnel on a 1/16-scale model of the McDo...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the Grumman AF-2S...
The effects of tail design on spin and recovery were investigated in a spin tunnel. A 1/11-scale mod...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
An investigation was conducted in the NASA Langley 20-Foot Vertical Spin Tunnel to determine the dev...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale ...
An investigation of the spin and recovery characteristics of a scale model of the Grumman XF9F-2 air...
An investigation of the spin and recovery characteristics of a 0.057-scale model of the Chance Vough...
Spin tests have been performed in the Langley 20-foot free-spinning tunnel on a 1/18-scale model of ...
This paper presents the results of a spin-tunnel investigation of a low-wing model typical of presen...
A supplementary investigation has been conducted in the Langley 20-foot free-spinning tunnel of a l/...
An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin a...
An investigation has been conducted in the Langley 20-foot free- spinning tunnel scale model of the ...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the eff...
Spin tests have been conducted in the Langley free-spinning tunnel on a 1/16-scale model of the McDo...
An investigation of the spin and recovery characteristics of a 1/24-scale model of the Grumman AF-2S...
The effects of tail design on spin and recovery were investigated in a spin tunnel. A 1/11-scale mod...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
An investigation was conducted in the NASA Langley 20-Foot Vertical Spin Tunnel to determine the dev...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale ...
An investigation of the spin and recovery characteristics of a scale model of the Grumman XF9F-2 air...
An investigation of the spin and recovery characteristics of a 0.057-scale model of the Chance Vough...
Spin tests have been performed in the Langley 20-foot free-spinning tunnel on a 1/18-scale model of ...
This paper presents the results of a spin-tunnel investigation of a low-wing model typical of presen...
A supplementary investigation has been conducted in the Langley 20-foot free-spinning tunnel of a l/...
An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin a...