This report, prepared at the request of NACA, gives the results of tests on a model propeller having blade sections with form of Gottingen airfoil no. 409. The model is shown to have a dynamic pitch practically equal to the nominal or geometrical pitch, and a somewhat higher efficiency but lower coefficient than would be expected of a propeller of more conventional sections
This report is the first of a series of four on propeller design and contains a description of the b...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Three airfoils, the N-85, the N-86, and the N-87, were tested at the request of the Bureau of Aerona...
This note describes tests of an adjustable blade metal model propeller, both in a free wind stream a...
This report presents the results of tests of a 4-foot model of Navy propeller No. 4412 in conjunctio...
The tests on these model propellers were undertaken for the purpose of determining the performance c...
Characteristics are given for the two-blade NACA 10-(3)(062)-045 propeller and for the two-blade NAC...
This report is a critical study of the results of propeller model tests with the view of obtaining a...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
This report presents the results of wind tunnel tests to determine the effect on the characteristics...
This report, prepared at the request of the NACA, describes tests of three metal model propellers, i...
This report contains artificial aerodynamic characteristics of a set of propeller sections to be use...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
Report presents the results of wind tunnel tests of propellers that examined the influence of the fo...
This report is the first of a series of four on propeller design and contains a description of the b...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Three airfoils, the N-85, the N-86, and the N-87, were tested at the request of the Bureau of Aerona...
This note describes tests of an adjustable blade metal model propeller, both in a free wind stream a...
This report presents the results of tests of a 4-foot model of Navy propeller No. 4412 in conjunctio...
The tests on these model propellers were undertaken for the purpose of determining the performance c...
Characteristics are given for the two-blade NACA 10-(3)(062)-045 propeller and for the two-blade NAC...
This report is a critical study of the results of propeller model tests with the view of obtaining a...
This report describes the tests of five adjustable blade metal model propellers both in a free wind ...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
This report presents the results of wind tunnel tests to determine the effect on the characteristics...
This report, prepared at the request of the NACA, describes tests of three metal model propellers, i...
This report contains artificial aerodynamic characteristics of a set of propeller sections to be use...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
Report presents the results of wind tunnel tests of propellers that examined the influence of the fo...
This report is the first of a series of four on propeller design and contains a description of the b...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
Three airfoils, the N-85, the N-86, and the N-87, were tested at the request of the Bureau of Aerona...