We can calculate the lift force by using the following equation
D=C
D½ ρ V
2 S
where
- D
- is Lift Force. [N]
- CD
- is Coefficient of Lift. [dimensionless]
- ½
- is the constant number a half. [dimensionless]
- ρ
- air density. [kg m-3]
- V2
- is the relative velocity of the air squared. [m2 s-2]
- S
- is the surface area of the object the air is travelling over.[m2]
The ½ρV2 term is also known as dynamic pressure.
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