The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 airplane were investigated in the Langley 8-foot transonic tunnel. The effect of speed brakes located at the end of the fuselage was also investigated. The main part of the investigation was made with internal flow in the model, but some data were obtained with no internal flow. The longitudinal stability and control at transonic-speeds appeared satisfactory. The transonic drag rise was small. The speed brakes had no adverse effects on longitudinal stability
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with f...
A wind-tunnel investigation was made to determine the longitudinal aerodynamic characteristics of a ...
An investigation was made by the NACA wing-flow method to determine the drag, pitching-moment, lift,...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
The effects of elevator deflections from 0deg to -20deg on the force and moment characteristics of a...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
A comprehensive investigation of the aerodynamic characteristics of various configurations of a 1/22...
The transonic longitudinal aerodynamic characteristics of a 0.0858-scale model of the Lockheed XF-10...
This report presents the results of an investigation in the transonic speed range of the longitudina...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
An investigation has teen made in the Langley high-speed 7- by 10-”foot tunnel using the trensonic-b...
The results of transonic flight measurements of the longitudinal stability characteristics of the Do...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
A test technique and data analysis method has been developed for determining the longitudinal aerody...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with f...
A wind-tunnel investigation was made to determine the longitudinal aerodynamic characteristics of a ...
An investigation was made by the NACA wing-flow method to determine the drag, pitching-moment, lift,...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
The effects of elevator deflections from 0deg to -20deg on the force and moment characteristics of a...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
A comprehensive investigation of the aerodynamic characteristics of various configurations of a 1/22...
The transonic longitudinal aerodynamic characteristics of a 0.0858-scale model of the Lockheed XF-10...
This report presents the results of an investigation in the transonic speed range of the longitudina...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
An investigation has teen made in the Langley high-speed 7- by 10-”foot tunnel using the trensonic-b...
The results of transonic flight measurements of the longitudinal stability characteristics of the Do...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
A test technique and data analysis method has been developed for determining the longitudinal aerody...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with f...
A wind-tunnel investigation was made to determine the longitudinal aerodynamic characteristics of a ...
An investigation was made by the NACA wing-flow method to determine the drag, pitching-moment, lift,...