The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-density tunnel have been reduced to a comparable form and are published in this report for convenient reference. Plots of the standard characteristics are given in tabular form. Included is a tabulation of important characteristics for the related airfoils reported in NACA report 460. This report, in conjunction with NACA report 610, makes available in comparable and convenient form the aerodynamic data for airfoils tested in the variable-density tunnel since January 1, 1931
This report gives the results of tests in the NACA full-scale and variable-density tunnels of a new ...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, a...
The results of an investigation of the effect of support interference on airfoil drag data obtained ...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The historical development of NACA airfoils is briefly reviewed. New data are presented that permit ...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
This report gives the results of tests in the NACA full-scale and variable-density tunnels of a new ...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
In order to give the large-scale characteristics of a variety of airfoils in a form which will be of...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, a...
The results of an investigation of the effect of support interference on airfoil drag data obtained ...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The historical development of NACA airfoils is briefly reviewed. New data are presented that permit ...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
This report gives the results of tests in the NACA full-scale and variable-density tunnels of a new ...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...