Add to ORKGAn investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of airplane models having a triangular wing and vertical tail surfaces. (author
Tests were made of an airplane model having a 45.1 degree swept-back wing with aspect ratio 2.50 and...
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of whic...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
An investigation was made to determine the effects of wing position and fuselage size on the low-spe...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
A low-scale wind-tunnel investigation was conducted in rolling flow to determine the effects of aspe...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Carrier landing-approach studies of a tailless delta-wing fighter airplane disclosed that approach s...
Low-speed tests of a model with a wing swept back 35 degrees at the 0.33-chord line and a horizontal...
Report presents the results of an investigation conducted in the Langley stability tunnel to determi...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
An. investigation was made to determine the effects of certical-tail size and length and of fuselage...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
An investigation has been made to determine the effect of Reynolds number on the lateral-stability d...
Tests were made of an airplane model having a 45.1 degree swept-back wing with aspect ratio 2.50 and...
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of whic...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
An investigation was made to determine the effects of wing position and fuselage size on the low-spe...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
A low-scale wind-tunnel investigation was conducted in rolling flow to determine the effects of aspe...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Carrier landing-approach studies of a tailless delta-wing fighter airplane disclosed that approach s...
Low-speed tests of a model with a wing swept back 35 degrees at the 0.33-chord line and a horizontal...
Report presents the results of an investigation conducted in the Langley stability tunnel to determi...
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-fl...
An. investigation was made to determine the effects of certical-tail size and length and of fuselage...
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fu...
An investigation has been made to determine the effect of Reynolds number on the lateral-stability d...
Tests were made of an airplane model having a 45.1 degree swept-back wing with aspect ratio 2.50 and...
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of whic...
Effect of vertical tails on low speed static stability characteristics of canard-bomber configuratio...