The forces acting on the blades of a propeller proceed from the mass of the propeller and the resistance of the surrounding medium. The magnitude, direction and point of application of the resultant to the propeller blade is of prime importance for the strength calculation. Since it was obviously impracticable to bring any kind of testing device near the revolving propeller, not so much on account of the element of danger as on account of the resulting considerable disturbance of the air flow, the deflection in both cases was photographically recorded and subsequently measured at leisure
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
A method is described for testing the strength of propellers of any shape. It is shown that the shap...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
The torsional deflection of the blades of three full-scale aluminum-alloy propellers operating under...
The present report deals with different vibration stresses of the propeller and their removal by an ...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Propellers with trailing-edge extensions were studied to determine aerodynamic characteristics. Trai...
The different kinds of energy losses of the propeller and the values of the constants determining th...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...
A method is described for testing the strength of propellers of any shape. It is shown that the shap...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
The torsional deflection of the blades of three full-scale aluminum-alloy propellers operating under...
The present report deals with different vibration stresses of the propeller and their removal by an ...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Propellers with trailing-edge extensions were studied to determine aerodynamic characteristics. Trai...
The different kinds of energy losses of the propeller and the values of the constants determining th...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
This report presents the results of full-scale tests made on a 10-foot 5-inch propeller on a geared ...