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Aircraft Airplane Wing Lift Design Equations and Formulas Calculator
Aerospace Aerodynamics
Solving For Lift Coefficient
Inputs:
Conversions:
| lift force (L) | = | 0 | = | 0 | newton | |
| density (p) | = | 0 | = | 0 | kilogram/meter^3 | |
| velocity (V) | = | 0 | = | 0 | meter/second | |
| surface area (A) | = | 0 | = | 0 | meter^2 |
Solution:
| lift coefficient (CL) | = | HAS NOT BEEN CALCULATED |
Other Units:
Change Equation
Select an equation to solve for a different unknown
Aircraft and airplane wing lift equations
Where
Select an equation to solve for a different unknown
Aircraft and airplane wing lift equations
 |
Solve for lift force |
 |
Solve for lift coefficient |
 |
Solve for air density |
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Solve for velocity |
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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.
AJ Design - Online Science Mathematics Engineering Software Programs | 2 | 3 | 4 | 5
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