Add to ORKGIn this report, the induced yawing moment, due to the rolling moment produced by the ailerons, is computed. This induced yawing moment is the greatest part of the entire yawing moment encountered by the wings
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
Stability derivatives have been computed for twisted wings of different plan forms that include vari...
Pressure-distribution tests were made on the 32-foot whirling arm of the Daniel Guggenheim Airship I...
The aerodynamical constants of an airplane necessary for the discussion of stability are partly obse...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
In this report, the induced yawing moment, due to the rolling moment produced by the ailerons, is co...
The present work investigates, on the basis of Prandtl's wing theory, the form of the lift distribut...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Ailerons described in references 1, 2, and 3, are summarized in the form of empirical equations whic...
In the following note, prepared for the National Advisory Committee for Aeronautics, this induction ...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
The magnitudes of the yawing moments produced by various parts of an airplane during spins have prev...
This report deals with the application of the airfoil and twisted wing theory to the calculation of ...
The effect of an aileron displacement on the distribution of the lift along the span is computed for...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
Stability derivatives have been computed for twisted wings of different plan forms that include vari...
Pressure-distribution tests were made on the 32-foot whirling arm of the Daniel Guggenheim Airship I...
The aerodynamical constants of an airplane necessary for the discussion of stability are partly obse...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
In this report, the induced yawing moment, due to the rolling moment produced by the ailerons, is co...
The present work investigates, on the basis of Prandtl's wing theory, the form of the lift distribut...
Wind-tunnel data are presented on the rate of change of yawing moment with sideslip for tests of 9 c...
Ailerons described in references 1, 2, and 3, are summarized in the form of empirical equations whic...
In the following note, prepared for the National Advisory Committee for Aeronautics, this induction ...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
The magnitudes of the yawing moments produced by various parts of an airplane during spins have prev...
This report deals with the application of the airfoil and twisted wing theory to the calculation of ...
The effect of an aileron displacement on the distribution of the lift along the span is computed for...
A low scale wind tunnel investigation was conducted in rolling flow to determine the effects of aspe...
Stability derivatives have been computed for twisted wings of different plan forms that include vari...
Pressure-distribution tests were made on the 32-foot whirling arm of the Daniel Guggenheim Airship I...