It is endeavored in this report to give a full outline of the problem of airplane stability and to classify the proposed solutions systematically. Longitudinal stability, which can be studied separately, is considered first. The combination of lateral and directional stabilities, which cannot be separated, will be dealt with later
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The stability analysis of an airplane while rolling is much more simplified to the extent that it ca...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
This report concerns the study of automatic stabilizers and extends it to include the control of the...
The effect of restraint in pitching introduced by an automatic pilot upon the longitudinal stability...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
In this report a study is made of the effect on longitudinal and lateral oscillations of an airplane...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The stability analysis of an airplane while rolling is much more simplified to the extent that it ca...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
This report concerns the study of automatic stabilizers and extends it to include the control of the...
The effect of restraint in pitching introduced by an automatic pilot upon the longitudinal stability...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
In this report a study is made of the effect on longitudinal and lateral oscillations of an airplane...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The stability analysis of an airplane while rolling is much more simplified to the extent that it ca...