Hitherto it has been generally assumed, in calculating the fall of an airplane, that the forces withstood by the latter were distributed uniformly throughout the whole length of the wing. In reality this is not the case and German engineers in particular are now assuming an elliptical distribution of the forces. The latter hypothesis has made it possible to carry out a certain number of calculations which have been verified by experiment
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
On of the most important characteristics of an airfoil is the rate of change of lift with angle of a...
In the present treatise, a convenient method will be indicated, which makes it possible to determine...
The effect of tapered ailerons on linearly tapered wings is theoretically determined. Four different...
A procedure which takes into account the aerodynamic span effect is given for the determination of t...
The present contribution is the sequel to a paper written by Messrs. R. Fuchs, L. Hopf, and H. Hambu...
The theory of the oscillating airfoil of infinite span with two-dimensional flow has been developed ...
This presentation on 1933 Prandtl applications to a small research UAV. We will discuss the implicat...
The chief defect of the investigations up to now was the assumption of a more or less arbitrary "mea...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
The object of this series of experiments was to determine the influence of the relative vertical pos...
Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of ...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
On of the most important characteristics of an airfoil is the rate of change of lift with angle of a...
In the present treatise, a convenient method will be indicated, which makes it possible to determine...
The effect of tapered ailerons on linearly tapered wings is theoretically determined. Four different...
A procedure which takes into account the aerodynamic span effect is given for the determination of t...
The present contribution is the sequel to a paper written by Messrs. R. Fuchs, L. Hopf, and H. Hambu...
The theory of the oscillating airfoil of infinite span with two-dimensional flow has been developed ...
This presentation on 1933 Prandtl applications to a small research UAV. We will discuss the implicat...
The chief defect of the investigations up to now was the assumption of a more or less arbitrary "mea...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
The object of this series of experiments was to determine the influence of the relative vertical pos...
Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of ...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
On of the most important characteristics of an airfoil is the rate of change of lift with angle of a...
In the present treatise, a convenient method will be indicated, which makes it possible to determine...