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Aircraft Mechanics
Lift to Drag Ratio at Maximum Endurance Prop in Range and Endurance Formulas
Lift to Drag Ratio at Maximum Endurance Prop is the ratio of lift to drag at which the plane can fly (or loiter) for maximum time. And is denoted by LDEmax
ratio prop
.
Formulas to find Lift to Drag Ratio at Maximum Endurance Prop in Range and Endurance
f
x
Lift to Drag for Maximum Endurance given Preliminary Endurance for Prop-Driven Aircraft
Go
Range and Endurance formulas that make use of Lift to Drag Ratio at Maximum Endurance Prop
f
x
Specific Fuel Consumption given Preliminary Endurance for Prop-Driven Aircraft
Go
List of variables in Range and Endurance formulas
f
x
Endurance of Aircraft
Go
f
x
Velocity for Maximum Endurance
Go
f
x
Specific Fuel Consumption
Go
f
x
Propeller Efficiency
Go
f
x
Weight at Start of Loiter Phase
Go
f
x
Weight at End of Loiter Phase
Go
FAQ
What is the Lift to Drag Ratio at Maximum Endurance Prop?
Lift to Drag Ratio at Maximum Endurance Prop is the ratio of lift to drag at which the plane can fly (or loiter) for maximum time.
Can the Lift to Drag Ratio at Maximum Endurance Prop be negative?
{YesorNo}, the Lift to Drag Ratio at Maximum Endurance Prop, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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