The optimum circulation distribution and hence the maximum theoretical thrust obtainable for contra-vanes fitted behind propellers is markedly dependent on the number of guide vanes. The outer portion of the vanes, even if projecting considerably beyond the edge of the propeller slipstream, still contribute appreciably to this theoretical gain of thrust. But, owing to the always existing friction of the vanes, the limit of the optimum vane length lies at relatively small diameters. A large hub unloads the vanes. Hence, the guide vanes are best attached to suitable parts of the bodies which would, in any case, be subjected to the slipstream
Though dissimilar, these two subjects have been united because they have some points in common. The ...
The different kinds of energy losses of the propeller and the values of the constants determining th...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
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 fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
The change of induced wing drag due to the field of flow of the propeller was analyzed quantitativel...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
Tests of an 8-blade contra-propeller of 32-inch diameter in combination with a 4-inch, 36-inch diame...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Given here is a brief review of the fundamental principles of the propeller slip-stream theory and i...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
Though dissimilar, these two subjects have been united because they have some points in common. The ...
The different kinds of energy losses of the propeller and the values of the constants determining th...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...
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 fundamental vortex theory for a single rotation propeller with a finite number of blades is revi...
The change of induced wing drag due to the field of flow of the propeller was analyzed quantitativel...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
In the slipstream behind a propeller there is a considerable amount of kinetic energy which has been...
Tests of an 8-blade contra-propeller of 32-inch diameter in combination with a 4-inch, 36-inch diame...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
Given here is a brief review of the fundamental principles of the propeller slip-stream theory and i...
In the present paper I shall not consider the problem of the best arrangement of airplane and propel...
The choice of the numbers of revolutions and of the diameter, the distribution of thrust, and the va...
Though dissimilar, these two subjects have been united because they have some points in common. The ...
The different kinds of energy losses of the propeller and the values of the constants determining th...
I am now proposing a method for the preliminary approximate calculation of the thrust distribution a...