An investigation has been conducted to determine the effects of configuration variables on the lateral-directional stability characteristics of a wing-fuselage configuration. The variables under study included variations in the location of a single center-line vertical tail and twin vertical tails, wing height, fuselage strakes, and horizontal tails. The study was conducted in the Langley high-speed 7-by 10-foot tunnel at a Mach number of 0.30, at angles of attack up to 44 deg and at sideslip angles of 0 deg and plus or minus 5 deg
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...
Low-speed, static wind-tunnel tests were conducted to explore the effects of fighter fuselage forebo...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
Subsonic lateral-direction and longitudinal characteristics of a forward-swept-wing fighter configur...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
The effects were studied of various vertical-tail configurations on the longitudinal and lateral dir...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Factors affecting static, longitudinal, and directional stability characteristics of supersonic airc...
A series of low-speed static wind-tunnel force tests were conducted on a 0.15-scale model of a moder...
A study was conducted to determine the longitudinal and lateral-directional aerodynamic characterist...
Tests were made in the Langley full-scale tunnel of the Grumman XF6f-4 airplane in order to investig...
The present paper summarizes the high-angle-of-attack characteristics of a number of high-performanc...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...
Low-speed, static wind-tunnel tests were conducted to explore the effects of fighter fuselage forebo...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
Subsonic lateral-direction and longitudinal characteristics of a forward-swept-wing fighter configur...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
The effects were studied of various vertical-tail configurations on the longitudinal and lateral dir...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Factors affecting static, longitudinal, and directional stability characteristics of supersonic airc...
A series of low-speed static wind-tunnel force tests were conducted on a 0.15-scale model of a moder...
A study was conducted to determine the longitudinal and lateral-directional aerodynamic characterist...
Tests were made in the Langley full-scale tunnel of the Grumman XF6f-4 airplane in order to investig...
The present paper summarizes the high-angle-of-attack characteristics of a number of high-performanc...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...
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