The tests described in this report were made in the 5-foot atmospheric wind tunnel of the National Advisory Committee for Aeronautics, at Langley Field. The primary objective of collecting data on the characteristics of this tunnel for comparison with those of others throughout the world, in order that, in the future, the results of tests made in all the principle laboratories may be interpreted, compared, and coordinated on a basis of scientifically established relationships, a process hitherto impossible due to the lack of comparable data. The work includes tests of a disk, spheres, cylinders, and airfoils, explorations of the test section for static pressure and velocity distribution, and determination of the variations of air flow direc...
Wind-Tunnel tests were conducted in the Lockheed-Georgia Company's compressible flow facility to det...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
This report gives a complete description of the full-scale wind tunnel of the National Advisory Comm...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
This report gives a description of the high-speed wind tunnel of the National Advisory Committee for...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
The results of an experimental investigation on the boundary-correction factor are presented in this...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
This report presents the results of force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Wind-Tunnel tests were conducted in the Lockheed-Georgia Company's compressible flow facility to det...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
This report gives a complete description of the full-scale wind tunnel of the National Advisory Comm...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
This report gives a description of the high-speed wind tunnel of the National Advisory Committee for...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
The results of an experimental investigation on the boundary-correction factor are presented in this...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
This report presents the results of force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Wind-Tunnel tests were conducted in the Lockheed-Georgia Company's compressible flow facility to det...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
This report gives a complete description of the full-scale wind tunnel of the National Advisory Comm...