In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been imparted to it by the engine without producing any corresponding propeller thrust. The increased absorption of power reduces the propeller efficiency. Attention has been previously directed to this question by Bendemann and Madelung and other writers. Their contribution serves to verify a simple method of calculating the reduction in the propeller efficiency due to the slip stream. That method of calculation is given here. Explanations and examples are given for as single propeller and for two propellers mounted in tandem
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report is an extension of NACA-TR-168 and has been prepared for the National Advisory Committee...
A simplified model is used to describe the interaction between a propeller slipstream and a wing in ...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
The change of induced wing drag due to the field of flow of the propeller was analyzed quantitativel...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The optimum circulation distribution and hence the maximum theoretical thrust obtainable for contra-...
The stipulation of best thrust distribution is applied to the annular elements of the screw propelle...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
The fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
An analysis is given which enables the design of dual-rotation propellers. It relies on the use of a...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
This report is an analysis of experiments performed by Eiffel on the air velocity in slip stream of ...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report is an extension of NACA-TR-168 and has been prepared for the National Advisory Committee...
A simplified model is used to describe the interaction between a propeller slipstream and a wing in ...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
The change of induced wing drag due to the field of flow of the propeller was analyzed quantitativel...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The optimum circulation distribution and hence the maximum theoretical thrust obtainable for contra-...
The stipulation of best thrust distribution is applied to the annular elements of the screw propelle...
The screw propeller on airplanes is usually placed near other objects, and hence its performance may...
The fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
An analysis is given which enables the design of dual-rotation propellers. It relies on the use of a...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
This report is an analysis of experiments performed by Eiffel on the air velocity in slip stream of ...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
This report is an extension of NACA-TR-168 and has been prepared for the National Advisory Committee...
A simplified model is used to describe the interaction between a propeller slipstream and a wing in ...