Force measurements giving total thrust and torque, and propeller slip stream surveys giving differential thrust and torque were simultaneously made on each of six full-scale propellers in the 20-foot propeller-research tunnel of the National Advisory Committee for Aeronautics. They were adjustable-pitch metal propellers 9.5 feet in diameter; three had modified Clark Y blade sections and three had modified RAF-6 blade sections. This report gives the differential thrust and torque and the variation caused by changing the propeller tip speed and the pitch setting. The total thrust and torque obtained from integration of the thrust and torque distribution curves are compared with those obtained by direct force measurements
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
This report presents the results of a series of negative thrust and torque measurements made with a ...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Negative thrust and torque data for 2, 3, and 4-blade metal propellers having Clark y and R.A.F. 6 a...
A set of propeller performance charts, based on a torque speed coefficient has been constructed from...
Static thrust and power measurements were made of six full-scale propellers. The propellers were mou...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Two 3-blade 10-foot propellers were operated in front of a liquid-cooled engine nacelle. The propell...
Force measurements giving total thrust and torque, and propeller slip stream surveys giving differen...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
This report presents the results of a series of negative thrust and torque measurements made with a ...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Negative thrust and torque data for 2, 3, and 4-blade metal propellers having Clark y and R.A.F. 6 a...
A set of propeller performance charts, based on a torque speed coefficient has been constructed from...
Static thrust and power measurements were made of six full-scale propellers. The propellers were mou...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Two 3-blade 10-foot propellers were operated in front of a liquid-cooled engine nacelle. The propell...
Force measurements giving total thrust and torque, and propeller slip stream surveys giving differen...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...