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 represents the rate at which the aircraft's engine consumes fuel to cover a certain distance while maintaining a specific lift-to-drag ratio, it measures the amount of fuel required per unit of distance traveled under the specified conditions. Specific Fuel Consumption 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 (LD), Gross Weight (W0) & Weight without fuel (W1) 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 -> 14688.04 = (0.93/7126)*(2.5)*(ln(5000/3000)).