Add to ORKGContains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow
An investigation was conducted in the Langley 8-foot high-speed tunnel to determine the effects of a...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of whic...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Contains low-speed longitudinal stability characteristics of a 52 degree sweptback wing of aspect ra...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
This investigation was made to determine the effects of 6 degree full-spoan and 3 degree partial-spa...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Results are given of a wind-tunnel investigation at a Reynolds number of 6.8 x 10(exp 6) to determin...
An investigation was conducted in the Langley 8-foot high-speed tunnel to determine the effects of a...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of whic...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Contains low-speed longitudinal stability characteristics of a 52 degree sweptback wing of aspect ra...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
This investigation was made to determine the effects of 6 degree full-spoan and 3 degree partial-spa...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Results are given of a wind-tunnel investigation at a Reynolds number of 6.8 x 10(exp 6) to determin...
An investigation was conducted in the Langley 8-foot high-speed tunnel to determine the effects of a...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...