A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft of the latter and performing the function of changing the direction of motion of the fluid filaments, which naturally tend to adopt a helicoidal form. This paper presents a consideration of the real advantage of counter-propellers on aircraft and the best shape of the blades. First, the author determines the possible energy absorption by the tangential increments. This process will be facilitated by the examination of the polygons of the relative velocities fore and aft of the generic section, of radius r, of one of the blades of the propeller
The stipulation of best thrust distribution is applied to the annular elements of the screw propelle...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
The optimum circulation distribution and hence the maximum theoretical thrust obtainable for contra-...
The forces acting on the blades of a propeller proceed from the mass of the propeller and the resist...
A numerical method has been developed using the techniques of Lock and Thaodonan as dasc&M hy Da...
Results are reported of a NASA sponsored analytical investigation into the merits of advanced counte...
Tests of an 8-blade contra-propeller of 32-inch diameter in combination with a 4-inch, 36-inch diame...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
A hydromechanical theory is developed for cycloidal propellers for two limiting modes of operation ...
The stipulation of best thrust distribution is applied to the annular elements of the screw propelle...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...
A counter-propeller is a fixed propeller smaller than the main propeller, mounted either fore or aft...
This note describes tests made at Stanford University on a four-blade fixed counter-propeller in com...
The optimum circulation distribution and hence the maximum theoretical thrust obtainable for contra-...
The forces acting on the blades of a propeller proceed from the mass of the propeller and the resist...
A numerical method has been developed using the techniques of Lock and Thaodonan as dasc&M hy Da...
Results are reported of a NASA sponsored analytical investigation into the merits of advanced counte...
Tests of an 8-blade contra-propeller of 32-inch diameter in combination with a 4-inch, 36-inch diame...
The different kinds of energy losses of the propeller and the values of the constants determining th...
The propeller cannot be considered alone, but the mutual interference between propeller and airplane...
The air flow and the air force created by all elements of the propeller blades lying in a ring locat...
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed...
A hydromechanical theory is developed for cycloidal propellers for two limiting modes of operation ...
The stipulation of best thrust distribution is applied to the annular elements of the screw propelle...
Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for struc...
Two screw propellers, a normal airplane propeller with a pitch/diameter ratio H/D = 0.5 and a helico...