Airplane Wing Lift Design Equation Calculator
Aircraft Aerospace Aerodynamics Formulas
Problem:
Solve for Surface Area
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Aircraft and airplane wing lift equations
 | Solve for lift force |
 | Solve for lift coefficient |
 | Solve for air density |
 | Solve for velocity |
 | Solve for lift surface area |
Where
| L | = | lift force |
| CL | = | lift coefficient |
| p | = | air density |
| V | = | velocity |
| A | = | lift surface area |
Reference - Books:
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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By Jimmy Raymond
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