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Aircraft Mechanics
Lift Coefficient in Range and Endurance Formulas
The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. And is denoted by C
L
.
Range and Endurance formulas that make use of Lift Coefficient
f
x
Endurance of Jet Airplane
Go
f
x
Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
Go
f
x
Range of Jet Airplane
Go
f
x
Thrust-Specific Fuel Consumption for given Range of Jet Airplane
Go
f
x
Breguet Endurance Equation
Go
f
x
Range of Propeller-Driven Airplane
Go
f
x
Propeller Efficiency for given Range of Propeller-Driven Airplane
Go
f
x
Specific Fuel Consumption for given Range of Propeller-Driven Airplane
Go
f
x
Endurance of Propeller-Driven Airplane
Go
f
x
Propeller Efficiency for given Endurance of Propeller-Driven Airplane
Go
f
x
Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
Go
FAQ
What is the Lift Coefficient?
The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Can the Lift Coefficient be negative?
{YesorNo}, the Lift Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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