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Aircraft Airplane Wing Lift Design Equations and Formulas Calculator

Aerospace Aerodynamics


Solving For Lift Force

Lift Force


Inputs:

coefficient of lift (CL)
density (p)
velocity (V)
surface area (A)



Conversions:

coefficient of lift (CL)
=0
=0
density (p)
=0
=0
kilogram/meter^3
velocity (V)
=0
=0
meter/second
surface area (A)
=0
=0
meter^2


Solution:

lift force (L)
=NOT CALCULATED 


Other Units:



Change Equation
Select an equation to solve for a different unknown

Aircraft and airplane wing lift equations
lift force Solve for lift force
lift coefficient Solve for lift coefficient
air density Solve for air density
velocity Solve for velocity
lift surface area Solve for lift surface area

Where
L  =  lift force
CL  =  lift coefficient 
p  =  air density 
V  =  velocity 
A  =  lift surface area


Reference - Books:

1) Munson, B.R., D. F. Young, and T. H. Okiishi. 1994. Fundamentals of Fluid Mechanics. John Wiley and Sons, Inc. 2nd ed.
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