In the present report, aerodynamic relations under the effect of the weight moments are investigated, and an example given of the computation of the stability for a practical case. Later, the effects of the masses of the controls on the dynamic longitudinal stability will be considered
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
In a recent Technical Note (NACA-TN-115, October, 1922), Norton and Carrol have reported experiments...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
The relation between the elevator hinge moment parameters and the control forces for changes in forw...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
The present report discusses three different systems of elevator control and their effects on the st...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
The discussion of the structural methods for obtaining lateral stability discloses the remarkable in...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a ...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
In a recent Technical Note (NACA-TN-115, October, 1922), Norton and Carrol have reported experiments...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
The relation between the elevator hinge moment parameters and the control forces for changes in forw...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
The present report discusses three different systems of elevator control and their effects on the st...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
The discussion of the structural methods for obtaining lateral stability discloses the remarkable in...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
The effects of mass distribution on lateral stability and control characteristics of an airplane hav...
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a ...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
In a recent Technical Note (NACA-TN-115, October, 1922), Norton and Carrol have reported experiments...
An investigation was made of the static longitudinal stability, and control and stall characteristic...