Add to ORKGA theoretical analysis is presented for obtaining, by use of Theodorsen's propeller theory, the load...
The vortex theory as presented by the author in earlier papers has been extended to permit the solut...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
A method was developed for the design of propellers of minimum induced loss matched to an arbitrary ...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
An analysis is given which enables the design of dual-rotation propellers. It relies on the use of a...
The fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
A description of the two swept propellers investigated in the Langley 8-foot high-speed tunnel is pr...
Full-scale measurements of shaft thrust and torque were made. Wind-tunnel speeds and blade angles we...
A theoretical analysis is presented for obtaining, by use of Theodorsen's propeller theory, the load...
The vortex theory as presented by the author in earlier papers has been extended to permit the solut...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
A method was developed for the design of propellers of minimum induced loss matched to an arbitrary ...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
An analysis is given which enables the design of dual-rotation propellers. It relies on the use of a...
The fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
Predicated on the assumption of certain normal conditions for engine and propeller, simple expressio...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
A description of the two swept propellers investigated in the Langley 8-foot high-speed tunnel is pr...
Full-scale measurements of shaft thrust and torque were made. Wind-tunnel speeds and blade angles we...
A theoretical analysis is presented for obtaining, by use of Theodorsen's propeller theory, the load...
The vortex theory as presented by the author in earlier papers has been extended to permit the solut...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...