Add to ORKGThis report describes and develops methods by which the aerodynamic characteristics of an airfoil may be calculated with sufficient accuracy for use in airplane design. These methods for prediction are based on the present aerodynamic theory and on empirical formulas derived from data obtained in the N. A. C. A. variable density wind tunnel at a Reynolds number corresponding approximately to full scale. (author)
From Summary: "Pressure distributions determined from high-speed wind-tunnel tests are presented for...
This report outlines the flight conditions that are usually critical in determining the design of co...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Report presents the results of an investigation of a systematically chosen representative group of r...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This report describes and develops methods by which the aerodynamic characteristics of an airfoil ma...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This collection of data on airfoils has been made from published reports of a number of the leading ...
Report presents methods of calculating air resistance of airfoils under certain conditions of flow p...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
From Summary: "Pressure distributions determined from high-speed wind-tunnel tests are presented for...
This report outlines the flight conditions that are usually critical in determining the design of co...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Report presents the results of an investigation of a systematically chosen representative group of r...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This report describes and develops methods by which the aerodynamic characteristics of an airfoil ma...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This collection of data on airfoils has been made from the published reports of a number of the lead...
This collection of data on airfoils has been made from published reports of a number of the leading ...
Report presents methods of calculating air resistance of airfoils under certain conditions of flow p...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
From Summary: "Pressure distributions determined from high-speed wind-tunnel tests are presented for...
This report outlines the flight conditions that are usually critical in determining the design of co...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...