Add to ORKGThis report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, and USA 45 airfoils as obtained from tests made in the Variable Density Wind Tunnel of the NACA. The results are given at both low and high Reynolds Numbers to show scale effect and to provide data for use in airplane design
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
"This report covers tests of a 5-foot model of the NACA 66,2-420 low-drag airfoil at high speeds inc...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
"This report covers tests of a 5-foot model of the NACA 66,2-420 low-drag airfoil at high speeds inc...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
"This report covers tests of a 5-foot model of the NACA 66,2-420 low-drag airfoil at high speeds inc...