Report presents the results of a series of 10-foot-diameter autogiro rotor models tested in the NACA 20-foot wind tunnel. Four of the models differed only in the airfoil sections of the blades, the sections used being the NACA 0012, 0018, 4412, and 4418. Three additional models employing the NACA 0012 section were tested, in which a varying portion of the blade near the hub was replaced by a streamline tube with a chord of about one-fourth the blade chord
Report presents an investigation carried out in the NACA 7- by 10-foot wind tunnel of an NACA 23012 ...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
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 force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
This report presents the results of wind-tunnel tests on a model gyroplane rotor 10 feet in diameter...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corru...
Report presents an investigation carried out in the NACA 7- by 10-foot wind tunnel of an NACA 23012 ...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
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 force tests on and air-flow surveys near PCA-2 autogiro rotor in...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
This report presents the results of wind-tunnel tests on a model gyroplane rotor 10 feet in diameter...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corru...
Report presents an investigation carried out in the NACA 7- by 10-foot wind tunnel of an NACA 23012 ...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...