Add to ORKGResults of flight tests of a control-feel aid presented. This device consisted of a spring and dashpot connected in series between the control stick and airplane structure. The device was tested in combination with an experimental elevator and bobweight which had given unsatisfactory dynamic stability and control-feel characteristics in previous tests. The control-feel aid effected marked improvement in both the control-feel characteristics and the control-feel dynamic longitudinal stability of the airplane
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The essential features of using pitch attitude for glidepath control in conjunction with longitudina...
A flight investigation was made to obtain experimental information on the handling qualities of a no...
Report presents the results of measurements of the longitudinal stability and control characteristic...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a ...
Data are presented showing the flight characteristics of a large airplane having a control-surface b...
A general study of longitudinal control feel was made with a transonic fighter-type airplane equippe...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashp...
The possibility of overshooting the anticipated normal acceleration as a result of the artificial-fe...
Report presents the results of measurements of the longitudinal stability and control characteristic...
In conjunction with a program of research on the general problem of stability of airplanes in the cl...
This investigation was carried out by the aerodynamic staff of the National Advisory Committee for A...
Tests were made to determine whether spring-tab ailerons tended to oscillate or flutter in speed ran...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The essential features of using pitch attitude for glidepath control in conjunction with longitudina...
A flight investigation was made to obtain experimental information on the handling qualities of a no...
Report presents the results of measurements of the longitudinal stability and control characteristic...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a ...
Data are presented showing the flight characteristics of a large airplane having a control-surface b...
A general study of longitudinal control feel was made with a transonic fighter-type airplane equippe...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashp...
The possibility of overshooting the anticipated normal acceleration as a result of the artificial-fe...
Report presents the results of measurements of the longitudinal stability and control characteristic...
In conjunction with a program of research on the general problem of stability of airplanes in the cl...
This investigation was carried out by the aerodynamic staff of the National Advisory Committee for A...
Tests were made to determine whether spring-tab ailerons tended to oscillate or flutter in speed ran...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The essential features of using pitch attitude for glidepath control in conjunction with longitudina...
A flight investigation was made to obtain experimental information on the handling qualities of a no...