Add to ORKGThe static longitudinal stability of an airplane with locked elevator is usually determined by analysis and model tests. The present report proposes to supply the results of such measurements. The method consisted of recording the dynamic pressure versus elevator displacement at different center-of-gravity positions in unaccelerated flight
In the present report, aerodynamic relations under the effect of the weight moments are investigated...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
These investigations consisted chiefly of measurements of the take-off distance under various starti...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
The static longitudinal stability of ad airplane with locked elevator is usually determined by analy...
The accuracy of the instruments used for flight test measurements has been inadequate so a new serie...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
1. In this particular airplane (Junkers F 13 ge) very minute changes in elevator displacement are eq...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
This investigation was carried out by the aerodynamic staff of the National Advisory Committee for A...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
In the present report, aerodynamic relations under the effect of the weight moments are investigated...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
These investigations consisted chiefly of measurements of the take-off distance under various starti...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
The static longitudinal stability of ad airplane with locked elevator is usually determined by analy...
The accuracy of the instruments used for flight test measurements has been inadequate so a new serie...
The rudder effect of a sport airplane at high angles of attack was to be improved. This made it nece...
For some time, the designers of airplanes have begun to occupy themselves with the question of longi...
1. In this particular airplane (Junkers F 13 ge) very minute changes in elevator displacement are eq...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
This investigation was carried out by the aerodynamic staff of the National Advisory Committee for A...
In the solution of a number of problems on the stability and controllability of airplanes, there ari...
In the present report, aerodynamic relations under the effect of the weight moments are investigated...
The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the...
These investigations consisted chiefly of measurements of the take-off distance under various starti...