Add to ORKGThis report provides a description of an automatic control mechanism that consists of an automatic e...
This report presents methods by which the cells of large commercial airplanes may be reduced. The ta...
The authors argue that the center of gravity has a preponderating influence on the longitudinal stab...
The control of an airplane is discussed beginning with sideways motion and following up with control...
Report presents the results of measurements of the longitudinal stability and control characteristic...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The directions and speed of development of plane avionics systems are determined by three factors: e...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
Our task is to endeavor to obtain precise experimental records of the motion of stalled airplanes, b...
This report is intended to furnish bases for load assumptions in the designing of airplane controls....
Measurements were made to determine the relative maximum forces a pilot can exert on the controls of...
Before undertaking a detailed description of an automatic-control mechanism, I will state briefly th...
The present trend is toward faster and larger pursuit airplanes. Because both speed and size increas...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashp...
This report provides a description of an automatic control mechanism that consists of an automatic e...
This report presents methods by which the cells of large commercial airplanes may be reduced. The ta...
The authors argue that the center of gravity has a preponderating influence on the longitudinal stab...
The control of an airplane is discussed beginning with sideways motion and following up with control...
Report presents the results of measurements of the longitudinal stability and control characteristic...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The directions and speed of development of plane avionics systems are determined by three factors: e...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
Our task is to endeavor to obtain precise experimental records of the motion of stalled airplanes, b...
This report is intended to furnish bases for load assumptions in the designing of airplane controls....
Measurements were made to determine the relative maximum forces a pilot can exert on the controls of...
Before undertaking a detailed description of an automatic-control mechanism, I will state briefly th...
The present trend is toward faster and larger pursuit airplanes. Because both speed and size increas...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashp...
This report provides a description of an automatic control mechanism that consists of an automatic e...
This report presents methods by which the cells of large commercial airplanes may be reduced. The ta...
The authors argue that the center of gravity has a preponderating influence on the longitudinal stab...