Add to ORKGThree groups of airfoils have been tested in the variable density wind tunnel. The first group contains three airfoils. The second group is a systematic series of twenty-seven airfoils. The third group consists of several frequently used wing sections
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
This report contains the results of a series of tests with three wing models. By changing the sectio...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
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 aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
Measurements were made in the variable density wind tunnel to determine the pressure distribution ov...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
A systematic series of 27 wing sections, characterized by a small travel of the center or pressure, ...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
This report contains the results of a series of tests with three wing models. By changing the sectio...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
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 aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
Measurements were made in the variable density wind tunnel to determine the pressure distribution ov...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
A systematic series of 27 wing sections, characterized by a small travel of the center or pressure, ...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...