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Aircraft Mechanics
Maximum Lift Coefficient in Take Off and Landing Formulas
Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack. And is denoted by C
L,max
.
Formulas to find Maximum Lift Coefficient in Take Off and Landing
f
x
Maximum Lift coefficient for given stall velocity
Go
f
x
Maximum Lift coefficient for given liftoff velocity
Go
Take Off and Landing formulas that make use of Maximum Lift Coefficient
f
x
Liftoff velocity for given weight
Go
f
x
Stall velocity for given weight
Go
f
x
Liftoff distance
Go
f
x
Thrust for given liftoff distance
Go
f
x
Landing ground roll distance
Go
f
x
Touchdown velocity
Go
List of variables in Take Off and Landing formulas
f
x
Weight
Go
f
x
Freestream Density
Go
f
x
Reference Area
Go
f
x
Stall Velocity
Go
f
x
Liftoff velocity
Go
FAQ
What is the Maximum Lift Coefficient?
Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.
Can the Maximum Lift Coefficient be negative?
{YesorNo}, the Maximum Lift Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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