Add to ORKGAn investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing. Longitudinal and lateral stability characteristics were obtained for the model with and without tail surfaces
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stabil...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of nega...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stabil...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of nega...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...