How to Calculate Range of Propeller-Driven Airplane?
Range of Propeller-Driven Airplane calculator uses Range of aircraft = (Propeller Efficiency/Specific Fuel Consumption)*(Lift Coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without fuel)) to calculate the Range of aircraft, The Range of Propeller-Driven Airplane is given by the Breguet range formula and is a function of propeller efficiency, specific fuel consumption, aerodynamic coefficients, gross weight, and weight without the fuel of aircraft. Range of aircraft is denoted by R symbol.
How to calculate Range of Propeller-Driven Airplane using this online calculator? To use this online calculator for Range of Propeller-Driven Airplane, enter Propeller Efficiency (η), Specific Fuel Consumption (c), Lift Coefficient (CL), Drag Coefficient (CD), Gross Weight (W0) & Weight without fuel (W1) and hit the calculate button. Here is how the Range of Propeller-Driven Airplane calculation can be explained with given input values -> 7126.017 = (0.93/0.000166666666666667)*(5/2)*(ln(5000/3000)).