The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the formulas, which afford an approximate solution, the unimportant effect of the height of the C.G. and the moment of the residual resistance are neglected. The effect of downwash from the forward horizontal empennage on the wing are also disregarded
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
A nomogram is developed which renders it possible by drawing a few lines, to determine: the location...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of c...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
This report is concerned with the problem of calculation of the horizontal tail area necessary to gi...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
It seems desirable to have some simple method for calculating quickly and with sufficient accuracy: ...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
A nomogram is developed which renders it possible by drawing a few lines, to determine: the location...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of c...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
This report is concerned with the problem of calculation of the horizontal tail area necessary to gi...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
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