Endurance of Propeller-Driven Airplane evaluator uses Endurance of Propeller Aircraft = Propeller Efficiency/Specific Fuel Consumption*(Lift Coefficient^1.5)/Drag Coefficient*sqrt(2*Freestream Density*Reference Area)*((1/Weight without Fuel)^(1/2)-(1/Gross Weight)^(1/2)) to evaluate the Endurance of Propeller Aircraft, Endurance of Propeller-Driven Airplane is a measure of the time an aircraft can stay aloft, which depends on factors such as propeller efficiency, specific fuel consumption, lift coefficient, drag coefficient, and aircraft weight. Endurance of Propeller Aircraft is denoted by Eprop symbol.
How to evaluate Endurance of Propeller-Driven Airplane using this online evaluator? To use this online evaluator for Endurance of Propeller-Driven Airplane, enter Propeller Efficiency (η), Specific Fuel Consumption (c), Lift Coefficient (CL), Drag Coefficient (CD), Freestream Density (ρ∞), Reference Area (S), Weight without Fuel (W1) & Gross Weight (W0) and hit the calculate button.