How to Calculate Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane?
Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane calculator uses Specific Fuel Consumption=(Propeller efficiency/Range of aircraft)*(Lift-to-drag ratio)*(ln(Gross Weight/Weight without fuel)) to calculate the Specific Fuel Consumption, The Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane is obtained from the Breguet range formula and is a function of propeller efficiency, gross weight, and weight without the fuel of aircraft. Specific Fuel Consumption and is denoted by c symbol.
How to calculate Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane using this online calculator? To use this online calculator for Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane, enter Propeller efficiency (η), Range of aircraft (R), Lift-to-drag ratio (L/D), Gross Weight (W_{0}) and Weight without fuel (W_{1}) and hit the calculate button. Here is how the Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane calculation can be explained with given input values -> 3.625E-5 = (0.93/100000)*(37)*(ln(5000/4500)).