The formula for calculating work done by an engine in one propeller revolution is: Work (in Joules) = Power (in Watts) x Time (in seconds).
The power output of an engine can be determined by multiplying the torque (in Newton-meters) by the rotational speed (in revolutions per minute) and dividing by 9.55 (conversion factor from horsepower to Watts). In this case, the power output would be: (527.612 N*m x 2310 RPM) / 9.55 = 12783.8 Watts or 17.1 horsepower.
The work done by an engine in one propeller revolution is a measure of the amount of energy that is transferred to the propeller to generate thrust. This can be used to determine the efficiency and performance of the engine and propeller system.
Yes, the work done by an engine in one propeller revolution can be increased by either increasing the power output of the engine, increasing the torque or rotational speed, or by optimizing the design of the propeller to reduce drag and increase efficiency.
The work done by an engine in one propeller revolution is directly related to the thrust generated by the propeller. This thrust, in turn, affects the speed and acceleration of an aircraft. A higher work output will result in greater thrust and therefore, increased speed and acceleration.