Zero-Lift Drag Coefficient at Minimum Thrust in Level Flight Formulas

The Zero-Lift Drag Coefficient at Minimum Thrust represents the drag coefficient of an aircraft when it is producing zero lift and operating at the minimum thrust required for level flight. And is denoted by C_D0,min.

Formulas to find Zero-Lift Drag Coefficient at Minimum Thrust in Level Flight

fxZero-lift drag coefficient at minimum required thrustGo

List of variables in Level Flight formulas

fx Lift Coefficient Go

fx Oswald Efficiency Factor Go

fx Aspect Ratio of a Wing Go

FAQ

What is the Zero-Lift Drag Coefficient at Minimum Thrust?

The Zero-Lift Drag Coefficient at Minimum Thrust represents the drag coefficient of an aircraft when it is producing zero lift and operating at the minimum thrust required for level flight.

Can the Zero-Lift Drag Coefficient at Minimum Thrust be negative?

{YesorNo}, the Zero-Lift Drag Coefficient at Minimum Thrust, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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