How to Calculate Range of Propeller-Driven Airplane for given lift-to-drag ratio?
Range of Propeller-Driven Airplane for given lift-to-drag ratio calculator uses Range of aircraft = (Propeller Efficiency/Specific Fuel Consumption)*(Lift-to-drag ratio)*(ln(Gross Weight/Weight without fuel)) to calculate the Range of aircraft, The Range of Propeller-Driven Airplane for given lift-to-drag ratio is obtained from the Breguet range formula and is a function of propeller efficiency, specific fuel consumption, 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 for given lift-to-drag ratio using this online calculator? To use this online calculator for Range of Propeller-Driven Airplane for given lift-to-drag ratio, enter Propeller Efficiency (η), Specific Fuel Consumption (c), Lift-to-drag ratio (LD), Gross Weight (W0) & Weight without fuel (W1) and hit the calculate button. Here is how the Range of Propeller-Driven Airplane for given lift-to-drag ratio calculation can be explained with given input values -> 48456.92 = (0.93/0.000166666666666667)*(2.5)*(ln(5000/3000)).