Add to ORKGMeasurements were made in the variable density wind tunnel to determine the pressure distribution over one section of a R.A.F. 31 airfoil with a leading edge slot fully open. To provide data for the study of scale effect on this type of airfoil, the tests were conducted with air densities of approximately one and twenty atmospheres
This report contains the results of a series of tests with three wing models. By changing the sectio...
This investigation was undertaken to study the distribution of loading over thick wings of various t...
Surface pressure distributions were measured for the 13% thick GA(W)-2 airfoil section fitted with 2...
Measurements were made in the variable density wind tunnel to determine the pressure distribution ov...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This report deals with pressure distribution tests on an airfoil with a conventional trailing edge f...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
Report presents the results of wind tunnel tests made in the NACA 7 by 10-foot wind tunnel of a Clar...
Report presents the results of a pressure-distribution investigation conducted in the Langley Memori...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
Report presents the results of pressure-distribution of an NACA 23012 airfoil equipped with a slotte...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Measurements were made to determine the distribution of pressure over one section of an R. A. F. 30 ...
Report presents the results of pressure-distribution tests of an NACA 23012 airfoil with an NACA 230...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This investigation was undertaken to study the distribution of loading over thick wings of various t...
Surface pressure distributions were measured for the 13% thick GA(W)-2 airfoil section fitted with 2...
Measurements were made in the variable density wind tunnel to determine the pressure distribution ov...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This report deals with pressure distribution tests on an airfoil with a conventional trailing edge f...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
Report presents the results of wind tunnel tests made in the NACA 7 by 10-foot wind tunnel of a Clar...
Report presents the results of a pressure-distribution investigation conducted in the Langley Memori...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
Report presents the results of pressure-distribution of an NACA 23012 airfoil equipped with a slotte...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Measurements were made to determine the distribution of pressure over one section of an R. A. F. 30 ...
Report presents the results of pressure-distribution tests of an NACA 23012 airfoil with an NACA 230...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This investigation was undertaken to study the distribution of loading over thick wings of various t...
Surface pressure distributions were measured for the 13% thick GA(W)-2 airfoil section fitted with 2...