Add to ORKGThis report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the National Advisory Committee for Aeronautics. Included also are calibration test results and characteristic test data of both static force tests and autorotation tests made in the tunnel
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
This report describes the Bucharest wind tunnel and presents numerous photographs and diagrams. The ...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous an...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
This report presents the results of wind tunnel tests on a Robinson-type anemometer. The investigati...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
The present report treats the subject of testing small models in a wind tunnel and of the methods em...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
This report describes the Bucharest wind tunnel and presents numerous photographs and diagrams. The ...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous an...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
This report presents the results of wind tunnel tests on a Robinson-type anemometer. The investigati...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
The present report treats the subject of testing small models in a wind tunnel and of the methods em...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
This report describes the Bucharest wind tunnel and presents numerous photographs and diagrams. The ...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...