This reports presents the results of measurements made of yawing moments produced by rudder displacement for seven rudders mounted on each of three fuselages at angles of pitch of 0 degree, 8 degrees, 12 degrees, 20 degrees, 30 degrees and 40 degrees. The dimensions of the rudders were selected to cover the range of areas and aspect ratios commonly used, while the ratios of rudder area to fin area and of rudder chord to fin chord were kept approximately constant. An important result of the measurements is to show that increased aspect ratio gives increased yawing moments for a given area, provided the maximum rudder displacement does not exceed 25 degrees. If large rudder displacements are used, the effect of aspect ratio is not so great
The aerodynamic forces and moments on a 1/12-scale model of the F4B-2 airplane were measured with th...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
Results are presented of a flight investigation conducted on a fighter-type airplane to determine th...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
This investigation was carried out by the National Advisory Committee for Aeronautics at the Langley...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The magnitudes of the yawing moments produced by various parts of an airplane during spins have prev...
This report presents the results of an investigation of the rolling and yawing moments due to ailero...
This report presents the results of an extension to higher angles of attack of the investigation of ...
The influence of airplane components, as well as wing location and tail length, on the rotational fl...
The influence of horizontal tail location on the rotational flow aerodynamics is discussed for a 1/6...
A flight investigation was made to determine the effect of various vertical-tail modifications and o...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
This investigation was undertaken to determine the relative effects of those factors which may inter...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
The aerodynamic forces and moments on a 1/12-scale model of the F4B-2 airplane were measured with th...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
Results are presented of a flight investigation conducted on a fighter-type airplane to determine th...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
This investigation was carried out by the National Advisory Committee for Aeronautics at the Langley...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The magnitudes of the yawing moments produced by various parts of an airplane during spins have prev...
This report presents the results of an investigation of the rolling and yawing moments due to ailero...
This report presents the results of an extension to higher angles of attack of the investigation of ...
The influence of airplane components, as well as wing location and tail length, on the rotational fl...
The influence of horizontal tail location on the rotational flow aerodynamics is discussed for a 1/6...
A flight investigation was made to determine the effect of various vertical-tail modifications and o...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
This investigation was undertaken to determine the relative effects of those factors which may inter...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
The aerodynamic forces and moments on a 1/12-scale model of the F4B-2 airplane were measured with th...
An investigation was made to determine the effects of vertical-tail size and length and of fuselage ...
Results are presented of a flight investigation conducted on a fighter-type airplane to determine th...