Add to ORKGA wind-tunnel investigation has been made at low speed to determine the effects of vertical fins placed ahead of the vertical tail on the directional stability and damping-in-yaw characteristics of a swept-wing model under steady-state oscillatory conditions. Various sizes of fins were used above and below the fuselage center line. The vertical-tail size also was varied
The paper presents a deep investigation on the methodologies to design a vertical tailplane. Nowaday...
A flight investigation was made to determine the effect of various vertical-tail modifications and o...
The object of the investigation described in this report was to compare the damping coefficients of ...
An experimental investigation has been made to determine the effects of vertical fins near the nose ...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
A wind-tunnel investigation has been made at low speed to determine the effects of vertical fins pla...
A discussion is given of the important aspects of the stalling of vertical tail surfaces. The type o...
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in ...
AbstractAgeneric aircraft with the single vertical tail usually lose its directional stability at me...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
Aircraft directional stability and control are related to vertical tail design. The safety, performa...
The paper presents a deep investigation on the aerodynamics of the vertical tailplane and the correc...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
The directional damping and stability of a fuselage- vertical-tail model oscillating freely in yaw w...
The paper presents a deep investigation on the methodologies to design a vertical tailplane. Nowaday...
A flight investigation was made to determine the effect of various vertical-tail modifications and o...
The object of the investigation described in this report was to compare the damping coefficients of ...
An experimental investigation has been made to determine the effects of vertical fins near the nose ...
Contributions of vertical tail and fuselage to directional stability are determined from pressure di...
A wind-tunnel investigation has been made at low speed to determine the effects of vertical fins pla...
A discussion is given of the important aspects of the stalling of vertical tail surfaces. The type o...
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in ...
AbstractAgeneric aircraft with the single vertical tail usually lose its directional stability at me...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
Aircraft directional stability and control are related to vertical tail design. The safety, performa...
The paper presents a deep investigation on the aerodynamics of the vertical tailplane and the correc...
Results are presented of a wind-tunnel investigation made to determine the influence of the fuselage...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
The directional damping and stability of a fuselage- vertical-tail model oscillating freely in yaw w...
The paper presents a deep investigation on the methodologies to design a vertical tailplane. Nowaday...
A flight investigation was made to determine the effect of various vertical-tail modifications and o...
The object of the investigation described in this report was to compare the damping coefficients of ...