The screw propeller on airplanes is usually placed near other objects, and hence its performance may be modified by them. Results of tests on propellers free from slip stream obstructions, both fore and aft, are therefore subject to correction, for the effect of such obstructions and the purpose of the investigation was to determine the effect upon the thrust and torque coefficients and efficiency, for previously tested air propellers, of obstructions placed in the slip stream, it being realized that such previous tests had been conducted under somewhat ideal conditions that are impracticable of realization in flight. Simple geometrical forms were used for the initial investigation. Such forms offered the advantage of easy, exact reproducti...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report contains the results of tests to determine the thrust (pull) and torque characteristics ...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
This investigation was undertaken to determine the relative effects of those factors which may inter...
The results of wind tunnel tests for the determination of the effect of a jet on the lift and downwa...
To quantify the installed performance of high speed (M = 0.8) turboprop propulsion systems, an exper...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
The effect of mutual propeller/nacelle of fuselage interference on aircraft propulsive efficiency is...
This report contains a description of a new and useful method suitable for the design of propellers ...
This work presents an experimental study of the effect of an installed propeller slipstream on a win...
The models designated "Torino 30, 31, 32" are horizontal tail surfaces of rectangular, triangular, a...
This report is an analysis of experiments performed by Eiffel on the air velocity in slip stream of ...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
This report is a critical study of the results of propeller model tests with the view of obtaining a...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report contains the results of tests to determine the thrust (pull) and torque characteristics ...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
This investigation was undertaken to determine the relative effects of those factors which may inter...
The results of wind tunnel tests for the determination of the effect of a jet on the lift and downwa...
To quantify the installed performance of high speed (M = 0.8) turboprop propulsion systems, an exper...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
The effect of mutual propeller/nacelle of fuselage interference on aircraft propulsive efficiency is...
This report contains a description of a new and useful method suitable for the design of propellers ...
This work presents an experimental study of the effect of an installed propeller slipstream on a win...
The models designated "Torino 30, 31, 32" are horizontal tail surfaces of rectangular, triangular, a...
This report is an analysis of experiments performed by Eiffel on the air velocity in slip stream of ...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
This report is a critical study of the results of propeller model tests with the view of obtaining a...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report contains the results of tests to determine the thrust (pull) and torque characteristics ...