Add to ORKGThe results of transonic flight measurements of the longitudinal stability characteristics of the Douglas D-558-II research airplane in the original configuration and with outboard fences mounted on the wings are presented. The levels of normal-force coefficient at which the stability decreases and pitch-up starts have been determined for both airplane configurations at Mach numbers up to about 0.94
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
Contains results of calculations made to determine the neutral oscillatory stability boundaries, per...
Wind tunnel tests of the 0.16-scale Douglas MX-656 model were made at low and high subsonic Mach num...
The results of transonic flight measurements of the longitudinal stability characteristics of the Do...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
This report presents the results of flight measurements of longitudinal stability and control charac...
During the flight program on the Bell X-5 airplane with 59 deg sweepback to determine the practical ...
The effects of elevator deflections from 0deg to -20deg on the force and moment characteristics of a...
An experimental investigation was made in the Langley stability tunnel to determine whether the low-...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
Flight measurements of the stability characteristics of the Bell X-5 research airplane at 59 deg swe...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
Contains results of calculations made to determine the neutral oscillatory stability boundaries, per...
Wind tunnel tests of the 0.16-scale Douglas MX-656 model were made at low and high subsonic Mach num...
The results of transonic flight measurements of the longitudinal stability characteristics of the Do...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
This report presents the results of flight measurements of longitudinal stability and control charac...
During the flight program on the Bell X-5 airplane with 59 deg sweepback to determine the practical ...
The effects of elevator deflections from 0deg to -20deg on the force and moment characteristics of a...
An experimental investigation was made in the Langley stability tunnel to determine whether the low-...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
Flight measurements of the stability characteristics of the Bell X-5 research airplane at 59 deg swe...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
Contains results of calculations made to determine the neutral oscillatory stability boundaries, per...
Wind tunnel tests of the 0.16-scale Douglas MX-656 model were made at low and high subsonic Mach num...