Add to ORKGWind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-thick airfoil designed for general aviation applications. The results were compared with NACA 12 percent-thick sections and with the 17 percent-thick NASA airfoil. The tests were conducted ovar a Mach number range from 0.10 to 0.35. Chord Reynolds numbers varied from about 2,000,000 to 9,000,000
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
In order to provide information that might lead to the development of better propeller section, 13 r...
An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional ...
Wind-tunnel tests have been conducted to determine the low-speed two-dimensional aerodynamic charact...
Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
Wind tunnel tests were conducted to determine the effects of airfoil thickness-ratio on the low spee...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
Wind-tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
A wind-tunnel test has been conducted in the Langley Low-Turbulence Pressure Tunnel to evaluate the ...
Tests were conducted in the Langley low-turbulence pressure tunnel to determine the aerodynamic char...
Low-speed wind-tunnel tests have been conducted to determine the two-dimensional aerodynamic charact...
Low speed sectional characteristics of a high lift airfoil are studied and a comparison is made of t...
Low speed wind tunnel tests were conducted to evaluate the effects on performance of modifying a 23 ...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
In order to provide information that might lead to the development of better propeller section, 13 r...
An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional ...
Wind-tunnel tests have been conducted to determine the low-speed two-dimensional aerodynamic charact...
Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
Wind tunnel tests were conducted to determine the effects of airfoil thickness-ratio on the low spee...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
Wind-tunnel tests were conducted to determine the low speed two dimensional aerodynamic characterist...
A wind-tunnel test has been conducted in the Langley Low-Turbulence Pressure Tunnel to evaluate the ...
Tests were conducted in the Langley low-turbulence pressure tunnel to determine the aerodynamic char...
Low-speed wind-tunnel tests have been conducted to determine the two-dimensional aerodynamic charact...
Low speed sectional characteristics of a high lift airfoil are studied and a comparison is made of t...
Low speed wind tunnel tests were conducted to evaluate the effects on performance of modifying a 23 ...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections ...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
In order to provide information that might lead to the development of better propeller section, 13 r...
An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional ...