Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go back to 1922. The object of the suction is chiefly to prevent the detachment of the boundary layer from the surface of the airfoil. At large angles of attack, such detachment prevents the attainment of the great lift promised by the theory, besides greatly increasing the drag, especially of thick airfoils. This report gives results of those experiments
An investigation was carried out in the NACA low-turbulence tunnel to develop low-drag airfoil secti...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Wind tunnel tests were conducted on airfoil models in order to study the flow separation phenomena o...
The present report deals with a series of tests made for the purpose of improving flow conditions ab...
The investigation was limited chiefly to the region of high angles of attack since it is only in thi...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
This report presents the results of the first investigation of the physical principle of preventing ...
The task of removing the boundary layer by suction consists in producing, in place of the ordinary f...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
The present report collects the investigations of the past years which, while not as yet intended fo...
The process of boundary layer control by means of suction is described. Its historical development i...
The basic ideas of a new method for treating the problem of the airfoil are presented, and a review ...
The results are presented of a triple series of tests using force measurements, pressure-distributio...
With an unsymmetrical wing and a rotating Magnus cylinder, the lift is produced by the superposition...
Several airfoils, Including a conventional NACA 23021 and some low-drag airfoils for which the thick...
An investigation was carried out in the NACA low-turbulence tunnel to develop low-drag airfoil secti...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Wind tunnel tests were conducted on airfoil models in order to study the flow separation phenomena o...
The present report deals with a series of tests made for the purpose of improving flow conditions ab...
The investigation was limited chiefly to the region of high angles of attack since it is only in thi...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
This report presents the results of the first investigation of the physical principle of preventing ...
The task of removing the boundary layer by suction consists in producing, in place of the ordinary f...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
The present report collects the investigations of the past years which, while not as yet intended fo...
The process of boundary layer control by means of suction is described. Its historical development i...
The basic ideas of a new method for treating the problem of the airfoil are presented, and a review ...
The results are presented of a triple series of tests using force measurements, pressure-distributio...
With an unsymmetrical wing and a rotating Magnus cylinder, the lift is produced by the superposition...
Several airfoils, Including a conventional NACA 23021 and some low-drag airfoils for which the thick...
An investigation was carried out in the NACA low-turbulence tunnel to develop low-drag airfoil secti...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Wind tunnel tests were conducted on airfoil models in order to study the flow separation phenomena o...