Results are presented of an investigation of stability, controllability, and stalling characteristics of five light airplanes. The effect of slots on the flying qualities of one of the airplanes is also shown. These five airplanes are considerd typical of the light airplanes now being manufactured.NACA TN No. 1573."May 1948."Includes bibliographical references.Results are presented of an investigation of stability, controllability, and stalling characteristics of five light airplanes. The effect of slots on the flying qualities of one of the airplanes is also shown. These five airplanes are considerd typical of the light airplanes now being manufactured.Mode of access: Internet
A compilation of the experimentally determined moments of inertia of 32 airplanes is presented. The ...
The present paper deals with flight test activities performed on light aircraft at University of Nap...
The present paper deals with flight test activities performed on light aircraft at University of Nap...
During October 1944, the National Advisory Committee for Aeronautics conducted a series of conferenc...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The National Advisory Committee for Aeronautics is undertaking an investigation of the flying qualit...
This investigation was made for the purpose of obtaining information on the maneuverability of the F...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The results of flight tests to determine flying qualities of a Chance Vought F4U-4 airplane are pres...
An investigation of a 1/7-scale powered model of the Kaiser Fleetwing all-wing airplane was made in ...
The material given in this report summarizes some of the results of recent research that will aid th...
The tests showed that a present day conventional airplane will fall into a spin when a turn is attem...
Flight measurements have been made to determine the characteristics of a pair of experimental ailero...
Data are presented showing the flight characteristics of a large airplane having a control-surface b...
"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet
A compilation of the experimentally determined moments of inertia of 32 airplanes is presented. The ...
The present paper deals with flight test activities performed on light aircraft at University of Nap...
The present paper deals with flight test activities performed on light aircraft at University of Nap...
During October 1944, the National Advisory Committee for Aeronautics conducted a series of conferenc...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The National Advisory Committee for Aeronautics is undertaking an investigation of the flying qualit...
This investigation was made for the purpose of obtaining information on the maneuverability of the F...
The effect of the characteristics of an airplane on balance, stability, and controllability, based o...
The results of flight tests to determine flying qualities of a Chance Vought F4U-4 airplane are pres...
An investigation of a 1/7-scale powered model of the Kaiser Fleetwing all-wing airplane was made in ...
The material given in this report summarizes some of the results of recent research that will aid th...
The tests showed that a present day conventional airplane will fall into a spin when a turn is attem...
Flight measurements have been made to determine the characteristics of a pair of experimental ailero...
Data are presented showing the flight characteristics of a large airplane having a control-surface b...
"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet
A compilation of the experimentally determined moments of inertia of 32 airplanes is presented. The ...
The present paper deals with flight test activities performed on light aircraft at University of Nap...
The present paper deals with flight test activities performed on light aircraft at University of Nap...