Add to ORKGThe present report deals with a series of tests made for the purpose of improving flow conditions about wings by applying the suction principle (increase of the lift coefficient and reduction of the drag about very thick wing sections). Though not conclusive, the report contains interesting results
Through the utilization of the "Magnus effect" on the Flettner rotor ship, the attention of the publ...
An investigation was undertaken to determine the increase in maximum lift coefficient that could be ...
The results are presented for visualization tests and measurements of the velocity field in diffusio...
The present report collects the investigations of the past years which, while not as yet intended fo...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
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...
With an unsymmetrical wing and a rotating Magnus cylinder, the lift is produced by the superposition...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
Even before the publication of the results of the Gottingen experiments on the removal of the bounda...
This report contains the results of a series of tests with three wing models. By changing the sectio...
In this report tests are described in which the distribution of pressures over models of the wings o...
The investigation was limited chiefly to the region of high angles of attack since it is only in thi...
Flight-test data and wind-tunnel data on suction profiles are substantially in agreement. The lift v...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Through the utilization of the "Magnus effect" on the Flettner rotor ship, the attention of the publ...
An investigation was undertaken to determine the increase in maximum lift coefficient that could be ...
The results are presented for visualization tests and measurements of the velocity field in diffusio...
The present report collects the investigations of the past years which, while not as yet intended fo...
Our attempts to improve the properties of airfoils by removing the boundary layer by suction, go bac...
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...
With an unsymmetrical wing and a rotating Magnus cylinder, the lift is produced by the superposition...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
Even before the publication of the results of the Gottingen experiments on the removal of the bounda...
This report contains the results of a series of tests with three wing models. By changing the sectio...
In this report tests are described in which the distribution of pressures over models of the wings o...
The investigation was limited chiefly to the region of high angles of attack since it is only in thi...
Flight-test data and wind-tunnel data on suction profiles are substantially in agreement. The lift v...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Through the utilization of the "Magnus effect" on the Flettner rotor ship, the attention of the publ...
An investigation was undertaken to determine the increase in maximum lift coefficient that could be ...
The results are presented for visualization tests and measurements of the velocity field in diffusio...