Add to ORKGWe are undertaking the task of computing the air forces on a slightly cambered airfoil in the absence of friction and with an infinite aspect ratio. We also assume in advance that the leading edge is very sharp and that its tangent lies in the direction of motion
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
A procedure is presented for obtaining the pressure distribution on an arbitrary airfoil section in ...
Theoretical pressure distributions on nonlifting circular-arc airfoils in two-dimensional flows with...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The basic ideas of a new method for treating the problem of the airfoil are presented, and a review ...
Low-aspect-ratio wings having pointed plan forms are treated on the assumption that the flow potenti...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
The well-known methods of thin-airfoil theory have been extended to oblique or sweptback airfoils of...
The aerodynamic characteristics of eight circular-arc airfoils at speeds of 0.5, 0.8, 0.95, and 1.08...
This report presents a solution of the problem of the theoretical flow of a frictionless incompressi...
Steady flow about curved airfoils is investigated analytically, first assuming air behaves as an ide...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
An airfoil is examined that has an upper surface shaped to control flow accelerations and pressure d...
A previous report gave calculations for the pressure distribution over thin oblique airfoils at supe...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
A procedure is presented for obtaining the pressure distribution on an arbitrary airfoil section in ...
Theoretical pressure distributions on nonlifting circular-arc airfoils in two-dimensional flows with...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The basic ideas of a new method for treating the problem of the airfoil are presented, and a review ...
Low-aspect-ratio wings having pointed plan forms are treated on the assumption that the flow potenti...
The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing exp...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
The well-known methods of thin-airfoil theory have been extended to oblique or sweptback airfoils of...
The aerodynamic characteristics of eight circular-arc airfoils at speeds of 0.5, 0.8, 0.95, and 1.08...
This report presents a solution of the problem of the theoretical flow of a frictionless incompressi...
Steady flow about curved airfoils is investigated analytically, first assuming air behaves as an ide...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
An airfoil is examined that has an upper surface shaped to control flow accelerations and pressure d...
A previous report gave calculations for the pressure distribution over thin oblique airfoils at supe...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
A procedure is presented for obtaining the pressure distribution on an arbitrary airfoil section in ...
Theoretical pressure distributions on nonlifting circular-arc airfoils in two-dimensional flows with...