This report describes an investigation made in order to determine the effect of tip speed on the characteristics of a thin-bladed metal propeller. The propeller was mounted on a VE-7 airplane with a 180-HP E-2 engine, and tested in the 20-foot propeller research tunnel of the National Advisory Committee for Aeronautics. It was found that the effect of tip speed on the propulsive efficiency was negligible within the range of the tests, which was from 600 to 1,000 feet per second (about 0.5 to 0.9 the velocity of sound in air). (author
This investigation is part of an extensive experimental study that has been carried out at full scal...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
Report presents the results of sound measurements at static conditions made for a two-blade 47-inch-...
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...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
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...
Tests were made of eight full-scale propellers of different shape at various tip speeds up to about ...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
A set of propeller performance charts, based on a torque speed coefficient has been constructed from...
Force measurements giving total thrust and torque, and propeller slip stream surveys giving differen...
This investigation is part of an extensive experimental study that has been carried out at full scal...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
Report presents the results of sound measurements at static conditions made for a two-blade 47-inch-...
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...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report describes in detail the new propeller research tunnel of the National Advisory Committee...
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...
Tests were made of eight full-scale propellers of different shape at various tip speeds up to about ...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
A set of propeller performance charts, based on a torque speed coefficient has been constructed from...
Force measurements giving total thrust and torque, and propeller slip stream surveys giving differen...
This investigation is part of an extensive experimental study that has been carried out at full scal...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
Report presents the results of sound measurements at static conditions made for a two-blade 47-inch-...
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