Add to ORKGThe aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional low-turbulence tunnels are presented. The data include lift, drag, and in some cases, pitching-moment characteristics, for Reynolds numbers between 3.0 x 10 (exp 6) and 9.0 x 10 (exp 6)
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characterist...
Two flight tests have been conducted that obtained extension pressure data on a modified AH-1G rotor...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
An investigation has been conducted in the Langley two-dimensional low--turbulence pressure tunnel t...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
An investigation has been conducted in the Langley low-turbulence pressure tunnel to determine the t...
Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This paper presents the results of wind-tunnel tests of several airfoils of low aspect ratio. The ai...
Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
An investigation was conducted in the Langley 6- by 28-inch transonic tunnel and the 6- by 19-inch t...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characterist...
Two flight tests have been conducted that obtained extension pressure data on a modified AH-1G rotor...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
An investigation has been conducted in the Langley two-dimensional low--turbulence pressure tunnel t...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
An investigation has been conducted in the Langley low-turbulence pressure tunnel to determine the t...
Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This paper presents the results of wind-tunnel tests of several airfoils of low aspect ratio. The ai...
Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
An investigation was conducted in the Langley 6- by 28-inch transonic tunnel and the 6- by 19-inch t...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characterist...
Two flight tests have been conducted that obtained extension pressure data on a modified AH-1G rotor...