How to Calculate Thrust-Specific Fuel Consumption for given Range of Jet Airplane?
Thrust-Specific Fuel Consumption for given Range of Jet Airplane calculator uses Thrust-Specific Fuel Consumption = (sqrt(8/(Freestream density*Reference Area)))*(1/(Range of aircraft*Drag Coefficient))*(sqrt(Lift Coefficient))*((sqrt(Gross Weight))-(sqrt(Weight without fuel))) to calculate the Thrust-Specific Fuel Consumption, The Thrust-Specific Fuel Consumption for given Range of Jet Airplane is a function of altitude, aerodynamic coefficients of lift & drag, and fuel weight. Thrust-Specific Fuel Consumption is denoted by ct symbol.
How to calculate Thrust-Specific Fuel Consumption for given Range of Jet Airplane using this online calculator? To use this online calculator for Thrust-Specific Fuel Consumption for given Range of Jet Airplane, enter Freestream density (ρ∞), Reference Area (S), Range of aircraft (R), Drag Coefficient (CD), Lift Coefficient (CL), Gross Weight (W0) & Weight without fuel (W1) and hit the calculate button. Here is how the Thrust-Specific Fuel Consumption for given Range of Jet Airplane calculation can be explained with given input values -> 36745.54 = (sqrt(8/(1.225*5.08)))*(1/(7126*2))*(sqrt(5))*((sqrt(5000))-(sqrt(3000))).