Add to ORKGWe have investigated the maximum lift obtainable with slotted airfoils derived from a symmetrical airfoil. These should have a smaller profile drag than other slotted airfoils
Tests of nine symmetrical airfoils, having different leading-edge radii, were made in the variable d...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
The present report is a description of systematic tests at maximum lift on airfoils with and without...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
Tests were made of an 0.309-chord double-slotted flap on an NACA 65, 3-118, a equals 1.0 airfoil sec...
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
This paper is the first of a series covering an investigation of a family of airfoils all formed fro...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Tests of nine symmetrical airfoils, having different leading-edge radii, were made in the variable d...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
The present report is a description of systematic tests at maximum lift on airfoils with and without...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
Tests were made of an 0.309-chord double-slotted flap on an NACA 65, 3-118, a equals 1.0 airfoil sec...
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
This paper is the first of a series covering an investigation of a family of airfoils all formed fro...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Tests of nine symmetrical airfoils, having different leading-edge radii, were made in the variable d...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...