Add to ORKGThe 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 presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
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 aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
Report presents the results of an investigation of a systematically chosen representative group of r...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
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 note is one of a series covering an investigation of a number of related airfoils. It presents ...
This report describes and develops methods by which the aerodynamic characteristics of an airfoil ma...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
From Summary: "Pressure distributions determined from high-speed wind-tunnel tests are presented for...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
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 aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
Report presents the results of an investigation of a systematically chosen representative group of r...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
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 note is one of a series covering an investigation of a number of related airfoils. It presents ...
This report describes and develops methods by which the aerodynamic characteristics of an airfoil ma...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
From Summary: "Pressure distributions determined from high-speed wind-tunnel tests are presented for...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Tests were carried out in the variable density wind tunnel of the National Advisory Committee for Ae...