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 and is denoted by c_{t} 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 (C_{D}), lift coefficient (C_{L}), Gross Weight (W_{0}) and Weight without fuel (W_{1}) 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 -> 1.311E-6 = (sqrt(8/(1.225*5)))*(1/(100000*100))*(sqrt(10))*((sqrt(5000))-(sqrt(4500))).