Add to ORKGIn the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing, aside from its freedom from autorotation,with respect to its polars and its construction, are taken into account as far as possible. It is indicated that the autorotation characteristics of a wing are dependent upon the speed of air flow as well as on the angle of yaw. This report postulates the knowledge of the behavior of certain conventional wings of different chords and cambers with respect to their air loads at large angles of attack
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
The problem of autorotation has been attacked by various authors, in particular Fuchs and Schmidt wh...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This report presents the results of a series of autorotation and torque tests on four different rota...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This article deals principally with Professor Bairstow's experiments on autorotation, in which the w...
This report describes the development of airplane characteristics since the war and indicates the di...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
An investigation was made to determine the spinning characteristics of Clark Y monoplane wings with ...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
The designing of an airplane requires an accurate knowledge of the aerodynamic properties of its win...
This reports presents the results of pressure distribution tests on a thick, tapered and twisted mon...
The present report deals with a number of problems, particularly with the interaction of the fuselag...
At the suggestion of Professor Betz, the following device was tested with the object of reducing the...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
The problem of autorotation has been attacked by various authors, in particular Fuchs and Schmidt wh...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This report presents the results of a series of autorotation and torque tests on four different rota...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This article deals principally with Professor Bairstow's experiments on autorotation, in which the w...
This report describes the development of airplane characteristics since the war and indicates the di...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
An investigation was made to determine the spinning characteristics of Clark Y monoplane wings with ...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
The designing of an airplane requires an accurate knowledge of the aerodynamic properties of its win...
This reports presents the results of pressure distribution tests on a thick, tapered and twisted mon...
The present report deals with a number of problems, particularly with the interaction of the fuselag...
At the suggestion of Professor Betz, the following device was tested with the object of reducing the...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
The problem of autorotation has been attacked by various authors, in particular Fuchs and Schmidt wh...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...