This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared J-5 engine and also on a similar 8-foot 11-inch propeller on a direct-drive J-5 engine. Each propeller was tested at two different pitch settings, and with a large and a small fuselage. The investigation was made in such a manner that the propeller-body interference factors were isolated, and it was found that, considering this interference only, the geared propellers had an appreciable advantage in propulsive efficiency, partially due to the larger diameter of the propellers with respect to the bodies, and partially because the geared propellers were located farther ahead of the engines and bodies
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
This report describes an investigation made in order to determine the effect of tip speed on the cha...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
This report describes an investigation made in order to determine the effect of tip speed on the cha...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
This report describes an investigation made in order to determine the effect of tip speed on the cha...