How to Calculate Specific Fuel Consumption for given Range of Propeller-Driven Airplane?
Specific Fuel Consumption for given Range of Propeller-Driven Airplane calculator uses Specific Fuel Consumption = (Propeller Efficiency/Range of aircraft)*(Lift Coefficient/Drag Coefficient)*(ln(Gross Weight/Weight without fuel)) to calculate the Specific Fuel Consumption, The Specific Fuel Consumption for given Range of Propeller-Driven Airplane is given by the Breguet range formula and is a function of propeller efficiency, range, aerodynamic coefficients, gross weight, and weight without the fuel of aircraft. Specific Fuel Consumption is denoted by c symbol.
How to calculate Specific Fuel Consumption for given Range of Propeller-Driven Airplane using this online calculator? To use this online calculator for Specific Fuel Consumption for given Range of Propeller-Driven Airplane, enter Propeller Efficiency (η), Range of aircraft (R), Lift Coefficient (CL), Drag Coefficient (CD), Gross Weight (W0) & Weight without fuel (W1) and hit the calculate button. Here is how the Specific Fuel Consumption for given Range of Propeller-Driven Airplane calculation can be explained with given input values -> 2788.947 = (0.93/7126)*(5/2)*(ln(5000/3000)).