Lift to Drag Ratio at Maximum Endurance in Aircraft Design Formulas

Lift to Drag Ratio at Maximum Endurance is the ratio of lift to drag at which the plane can fly (or Loiter) for maximum time. And is denoted by LDEmax_ratio.

Aircraft Design formulas that make use of Lift to Drag Ratio at Maximum Endurance

fxPreliminary Endurance for Prop-Driven AircraftGo

fxVelocity at Maximum Endurance given Preliminary Endurance for Prop-Driven AircraftGo

FAQ

What is the Lift to Drag Ratio at Maximum Endurance?

Lift to Drag Ratio at Maximum Endurance 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 be negative?

{YesorNo}, the Lift to Drag Ratio at Maximum Endurance, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

Let Others Know

✖

Facebook

Twitter

Copied!