Add to ORKGAt the suggestion of Professor Betz, the following device was tested with the object of reducing the autorotational speed of airplane wings. The model of a normal wing with the Gottigen profile 420, 1 meter span and 0.2 meter chord was provided with a pair of symmetrical slots on the suction side, connected with each other inside the wing. The arrangement of the testing equipment and models are given and the effect of the slots can be seen in the experimental curves that are included
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The apparatus consists of a universal balance with transmission at variable speeds from 300 to 5,000...
Tests were made with ordinary ailerons and different sizes of spoilers on rectangular Clark Y wing m...
At the suggestion of Professor Betz, the following device was tested with the object of reducing the...
For some time the D.V.L. has been investigating the question of applicability of Handley Page slotte...
For some time the D.V.L. has been investigating the question of applicability of Handley Page slotte...
Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotati...
The experiments herein described were made for the purpose of finding whether removing a larger port...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
This investigation was undertaken to develop a low-drag fixed slot for an airplane wing which would ...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Tests have been made in the NACA 7 by 10 foot wind tunnel on a Clark Y wing model equipped with vari...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This report presents the results of an investigation conducted in the NACA 7 by 10-foot wind tunnel ...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The apparatus consists of a universal balance with transmission at variable speeds from 300 to 5,000...
Tests were made with ordinary ailerons and different sizes of spoilers on rectangular Clark Y wing m...
At the suggestion of Professor Betz, the following device was tested with the object of reducing the...
For some time the D.V.L. has been investigating the question of applicability of Handley Page slotte...
For some time the D.V.L. has been investigating the question of applicability of Handley Page slotte...
Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotati...
The experiments herein described were made for the purpose of finding whether removing a larger port...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
This investigation was undertaken to develop a low-drag fixed slot for an airplane wing which would ...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Tests have been made in the NACA 7 by 10 foot wind tunnel on a Clark Y wing model equipped with vari...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This report presents the results of an investigation conducted in the NACA 7 by 10-foot wind tunnel ...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The apparatus consists of a universal balance with transmission at variable speeds from 300 to 5,000...
Tests were made with ordinary ailerons and different sizes of spoilers on rectangular Clark Y wing m...