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Aircraft Mechanics
Maximum Lift-to-Drag Ratio in Range and Endurance Formulas
The Maximum Lift-to-Drag Ratio is the highest ratio of lift force to drag force that an aircraft can achieve. And is denoted by LDmax
ratio
.
Formulas to find Maximum Lift-to-Drag Ratio in Range and Endurance
f
x
Maximum Lift to Drag Ratio given Preliminary Endurance for Jet Aircraft
Go
f
x
Maximum Lift to Drag Ratio given Range for Prop-Driven Aircraft
Go
f
x
Maximum Lift to Drag Ratio given Lift to Drag Ratio for Max Endurance of Prop-Driven Aircraft
Go
Range and Endurance formulas that make use of Maximum Lift-to-Drag Ratio
f
x
Cruise Weight Fraction for Jet Aircraft
Go
f
x
Specific Fuel Consumption given Range for Jet Aircraft
Go
f
x
Specific Fuel Consumption given Preliminary Endurance for Jet Aircraft
Go
f
x
Loiter Weight Fraction for Jet Aircraft
Go
f
x
Lift to Drag Ratio for Maximum Endurance given Max Lift to Drag Ratio for Prop-Driven Aircraft
Go
f
x
Propeller Efficiency given Range for Prop-Driven Aircraft
Go
f
x
Specific Fuel Consumption given Range for Prop-Driven Aircraft
Go
f
x
Cruise Weight Fraction for Prop-Driven Aircraft
Go
List of variables in Range and Endurance formulas
f
x
Endurance of Aircraft
Go
f
x
Specific Fuel Consumption
Go
f
x
Weight at Start of Loiter Phase
Go
f
x
Weight at End of Loiter Phase
Go
f
x
Range of Propeller Aircraft
Go
f
x
Propeller Efficiency
Go
f
x
Weight at Start of Cruise Phase
Go
f
x
Weight at End of Cruise Phase
Go
f
x
Lift to Drag Ratio at Maximum Endurance
Go
FAQ
What is the Maximum Lift-to-Drag Ratio?
The Maximum Lift-to-Drag Ratio is the highest ratio of lift force to drag force that an aircraft can achieve.
Can the Maximum Lift-to-Drag Ratio be negative?
{YesorNo}, the Maximum Lift-to-Drag Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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