Add to ORKGThe results of tests of six airfoils having the N.A.C.A. 230 mean line and varying in thickness from 0.06c to 0.21c are presented. These results agree with previous findings in showing that aerodynamically the best section is one of moderate thickness. The data are of value mainly in connection with the design of tapered wings having sections based on the N.A.C.A. 230 mean line
Section characteristics for use in wing design are presented for the NACA 23012 airfoil with plain a...
This paper is the first of a series covering an investigation of a family of airfoils all formed fro...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
This report gives the results of tests in the NACA full-scale and variable-density tunnels of a new ...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
Report presents the results of wind tunnel tests on a group of eight very thick airfoils having sect...
The results of tests of six airfoils having the N.A.C.A. 230 mean line and varying in thickness from...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Section characteristics for use in wing design are presented for the NACA 23012 airfoil with plain a...
This paper is the first of a series covering an investigation of a family of airfoils all formed fro...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
This report gives the results of tests in the NACA full-scale and variable-density tunnels of a new ...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
Report presents the results of wind tunnel tests on a group of eight very thick airfoils having sect...
The results of tests of six airfoils having the N.A.C.A. 230 mean line and varying in thickness from...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Section characteristics for use in wing design are presented for the NACA 23012 airfoil with plain a...
This paper is the first of a series covering an investigation of a family of airfoils all formed fro...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...