Add to ORKGTypical models and the testing technique used in the NACA free-spinning wind tunnel are described in detail. The results of tests on two models afford a comparison between the spinning characteristics of scale models in the tunnel and of the airplanes that they represent
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
This report presents the results of force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
Report presents the results of a series of 10-foot-diameter autogiro rotor models tested in the NACA...
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independentl...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
Report presents the results of tests of a 1/10-scale model of the XN2Y-1 airplane tested in the NACA...
The reported tests are a continuation of an NACA investigation being made in the free-spinning wind ...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
The tests described in this report were made in the 5-foot atmospheric wind tunnel of the National A...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
This report gives a description of the high-speed wind tunnel of the National Advisory Committee for...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
This report presents the results of force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
Report presents the results of a series of 10-foot-diameter autogiro rotor models tested in the NACA...
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independentl...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
Report presents the results of tests of a 1/10-scale model of the XN2Y-1 airplane tested in the NACA...
The reported tests are a continuation of an NACA investigation being made in the free-spinning wind ...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
The tests described in this report were made in the 5-foot atmospheric wind tunnel of the National A...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
This report gives a description of the high-speed wind tunnel of the National Advisory Committee for...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
This report presents the results of force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...