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Aircraft Mechanics
Coefficient Of Drag Due to Lift in Level Flight Formulas
The Coefficient of Drag Due to Lift represents the contribution of lift-induced drag to the total drag experienced by an aircraft. And is denoted by C
D,i
.
Formulas to find Coefficient Of Drag Due to Lift in Level Flight
f
x
Lift-Induced Drag Coefficient given required Thrust
Go
f
x
Coefficient of Drag due to Lift for Minimum Power required
Go
Level Flight formulas that make use of Coefficient Of Drag Due to Lift
f
x
Zero-Lift Drag Coefficient given required Thrust
Go
f
x
Zero-Lift Drag Coefficient for Minimum Power required
Go
f
x
Minimum Thrust of aircraft required
Go
List of variables in Level Flight formulas
f
x
Thrust
Go
f
x
Dynamic Pressure
Go
f
x
Reference Area
Go
f
x
Zero Lift Drag Coefficient
Go
FAQ
What is the Coefficient Of Drag Due to Lift?
The Coefficient of Drag Due to Lift represents the contribution of lift-induced drag to the total drag experienced by an aircraft.
Can the Coefficient Of Drag Due to Lift be negative?
{YesorNo}, the Coefficient Of Drag Due to Lift, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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