Airplane Aircraft Wing Lift Design Equations and Formulas Calculator
Aerospace Aerodynamics
Solving For Lift Force
Inputs:
Conversions:
| CL | = | 0 | | = | 0 | |
| p | = | 0 | | = | 0 | kilogram/meter^3 |
| V | = | 0 | | = | 0 | meter/second |
| A | = | 0 | | = | 0 | meter^2 |
Solution:
| lift force (L) | = | HAS NOT BEEN CALCULATED | |
Other Units:
| 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.
