Add to ORKGThis report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA ...
Report presents the results of a wind-tunnel investigation of the effect of wing-fuselage interferen...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
In connection with the interference program being conducted in the NACA variable-density wind tunnel...
Report presents results of wind tunnel tests of cambered aerofoils and body-wing combinations used f...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
Report presents the results of an investigation of a systematically chosen representative group of r...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This report presents the results of wind tunnel tests on a Mcdonnell Douglas airplane to determine t...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA ...
Report presents the results of a wind-tunnel investigation of the effect of wing-fuselage interferen...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
In connection with the interference program being conducted in the NACA variable-density wind tunnel...
Report presents results of wind tunnel tests of cambered aerofoils and body-wing combinations used f...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
Report presents the results of an investigation of a systematically chosen representative group of r...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
This report presents the results of wind tunnel tests on a Mcdonnell Douglas airplane to determine t...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
