Add to ORKGIt is possible to give a propeller such a shape that, under given conditions, viz., a definite speed of revolution and flying speed, the bending stresses in the blades will assume quite an insignificant magnitude
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
A description is given of the methods used in design of Micarta propellers. The most direct method f...
A method is described for testing the strength of propellers of any shape. It is shown that the shap...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
The forces acting on the blades of a propeller proceed from the mass of the propeller and the resist...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The advantages of the Kirsten-Boeing propeller consist essentially in the adjustability of the thrus...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
A description is given of the methods used in design of Micarta propellers. The most direct method f...
A method is described for testing the strength of propellers of any shape. It is shown that the shap...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
The forces acting on the blades of a propeller proceed from the mass of the propeller and the resist...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
Tests were conducted in order to determine how the characteristics of a propeller are affected by cu...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The advantages of the Kirsten-Boeing propeller consist essentially in the adjustability of the thrus...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
In order to determine the maximum and the most favorable pitch for a propeller, it was found desirab...
A description is given of the methods used in design of Micarta propellers. The most direct method f...