Add to ORKGData are presented showing compliance of C-54D with Army and Navy lateral and directional stability and control specifications. The airplane met requirements except for the rolling effectiveness pb/2V, the aileron forces in rolling, and the rudder forces in the asymmetric power conditions which were marginal. Also, the results of special tests concerning asymmetric power, asymmetric loading, and pitch due to yaw requested by the Airplane Handling Qualities Subcommittee of the Air Transport Association are presented
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Because the results of preliminary flight tests had indicated. the P-63A-1 airplane possessed insuff...
This paper presents the results of flight tests to determine the lateral and directional stability a...
Flight tests of a P-51H airplane with two different vertical-tail assemblies were made to determine ...
Data are presented showing compliance of C-54D with Army and Navy lateral and directional stability ...
Flight tests of a P-51H airplane with two different vertical-tail assemblies were made to determine ...
Report presents the results of an analysis made of the aileron control characteristics of numerous a...
Carrier landing-approach studies of a tailless delta-wing fighter airplane disclosed that approach s...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
The effects of large variations of lateral area on the lateral stability and control characteristics...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
The data presented have no bearing on performance characteristics of airplane, which were considered...
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...
At the request of the Air Materiel Command, Army Air Forces, flight tests were conducted on a P-5lD-...
Lateral-directional handling qualities survey to develop technique for predicting pilot rating
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Because the results of preliminary flight tests had indicated. the P-63A-1 airplane possessed insuff...
This paper presents the results of flight tests to determine the lateral and directional stability a...
Flight tests of a P-51H airplane with two different vertical-tail assemblies were made to determine ...
Data are presented showing compliance of C-54D with Army and Navy lateral and directional stability ...
Flight tests of a P-51H airplane with two different vertical-tail assemblies were made to determine ...
Report presents the results of an analysis made of the aileron control characteristics of numerous a...
Carrier landing-approach studies of a tailless delta-wing fighter airplane disclosed that approach s...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
The effects of large variations of lateral area on the lateral stability and control characteristics...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
The data presented have no bearing on performance characteristics of airplane, which were considered...
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...
At the request of the Air Materiel Command, Army Air Forces, flight tests were conducted on a P-5lD-...
Lateral-directional handling qualities survey to develop technique for predicting pilot rating
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Because the results of preliminary flight tests had indicated. the P-63A-1 airplane possessed insuff...
This paper presents the results of flight tests to determine the lateral and directional stability a...