Lift-to-Drag Ratio in Range and Endurance Formulas

The Lift-to-Drag Ratio is the amount of lift generated by a wing or vehicle, divided by the aerodynamic drag it creates by moving through the air. And is denoted by LD.

Formulas to find Lift-to-Drag Ratio in Range and Endurance

fxLift-to-Drag Ratio for given Endurance of Jet AirplaneGo

fxLift-to-Drag ratio for given Range of Propeller-Driven AirplaneGo

Range and Endurance formulas that make use of Lift-to-Drag Ratio

fxEndurance for given Lift-to-Drag Ratio of Jet AirplaneGo

fxThrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag Ratio of Jet AirplaneGo

fxBreguet RangeGo

fxRange of Propeller-Driven Airplane for given lift-to-drag ratioGo

fxPropeller Efficiency for given Range and Lift-to-Drag Ratio of Propeller-Driven AirplaneGo

fxSpecific Fuel Consumption for given Range and Lift-to-Drag Ratio of Propeller-Driven AirplaneGo

List of variables in Range and Endurance formulas

fx Thrust-Specific Fuel Consumption Go

fx Endurance of Aircraft Go

fx Gross Weight Go

fx Weight without Fuel Go

fx Specific Fuel Consumption Go

fx Range of Propeller Aircraft Go

fx Propeller Efficiency Go

Lift-to-Drag Ratio in Range and Endurance Formulas

Formulas to find Lift-to-Drag Ratio in Range and Endurance

Range and Endurance formulas that make use of Lift-to-Drag Ratio

List of variables in Range and Endurance formulas

FAQ