Add to ORKGThe present report discusses three different systems of elevator control and their effects on the stability and maneuverability of autogiros: (a) ailerons and elevators (standard); (b) blade control (la Cierval); (c) gravity control (new)
The development of more efficient control surfaces requiring less force to operate are presented
This report presents the results of flight test of the Pitcairn "PCA-2" autogiro. Lift and drag coef...
The effect of restraint in pitching introduced by an automatic pilot upon the longitudinal stability...
This report concerns the study of automatic stabilizers and extends it to include the control of the...
In the present report, aerodynamic relations under the effect of the weight moments are investigated...
The present report discusses three different systems of elevator control and their effects on the st...
The directions and speed of development of plane avionics systems are determined by three factors: e...
This report lays more stress on the principles underlying automatic piloting than on the means of ap...
Before undertaking a detailed description of an automatic-control mechanism, I will state briefly th...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
This report presents the results of tests in which the pressure distribution over the fixed wing of ...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The present report deals with a number of the main problems requiring solution in the development of...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The development of more efficient control surfaces requiring less force to operate are presented
This report presents the results of flight test of the Pitcairn "PCA-2" autogiro. Lift and drag coef...
The effect of restraint in pitching introduced by an automatic pilot upon the longitudinal stability...
This report concerns the study of automatic stabilizers and extends it to include the control of the...
In the present report, aerodynamic relations under the effect of the weight moments are investigated...
The present report discusses three different systems of elevator control and their effects on the st...
The directions and speed of development of plane avionics systems are determined by three factors: e...
This report lays more stress on the principles underlying automatic piloting than on the means of ap...
Before undertaking a detailed description of an automatic-control mechanism, I will state briefly th...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
This report presents the results of tests in which the pressure distribution over the fixed wing of ...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The present report deals with a number of the main problems requiring solution in the development of...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The development of more efficient control surfaces requiring less force to operate are presented
This report presents the results of flight test of the Pitcairn "PCA-2" autogiro. Lift and drag coef...
The effect of restraint in pitching introduced by an automatic pilot upon the longitudinal stability...