Add to ORKGAerodynamic tests were made with four geometrically similar metal propellers of different diameters, on a Wright "Whirlwind" J-5 engine in an open cockpit fuselage. The results show little difference in the characteristics of the various propellers, the only one of any importance being an increase of efficiency of the order of 1 per cent for a 5 per cent increase of diameter, within the range of the tests
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This investigation covers force tests through a large range of angle of attack on a series of monopl...