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Aircraft Mechanics
Zero Lift Drag Coefficient in Level Flight Formulas
Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift. And is denoted by C
D,0
.
Formulas to find Zero Lift Drag Coefficient in Level Flight
f
x
Zero-Lift Drag Coefficient given required Thrust
Go
f
x
Zero-Lift Drag Coefficient for given Lift Coefficient
Go
f
x
Zero-Lift Drag Coefficient for Minimum Power required
Go
Level Flight formulas that make use of Zero Lift Drag Coefficient
f
x
Lift-Induced Drag Coefficient given required Thrust
Go
f
x
Lift Coefficient given Minimum required Thrust
Go
f
x
Coefficient of Drag due to Lift for Minimum Power required
Go
f
x
Minimum Thrust of aircraft required
Go
f
x
Minimum Thrust required for given Lift Coefficient
Go
f
x
Minimum Thrust required for given weight
Go
List of variables in Level Flight formulas
f
x
Thrust
Go
f
x
Dynamic Pressure
Go
f
x
Reference Area
Go
f
x
Coefficient Of Drag Due to Lift
Go
f
x
Area
Go
f
x
Lift Coefficient
Go
f
x
Oswald Efficiency Factor
Go
f
x
Aspect Ratio of a Wing
Go
FAQ
What is the Zero Lift Drag Coefficient?
Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift.
Can the Zero Lift Drag Coefficient be negative?
{YesorNo}, the Zero Lift Drag Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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