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Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow. Check FAQs
FL=F-FD
FL - Lift Force?F - Aerodynamic Force?FD - Drag Force?

Lift given aerodynamic force Example

With values
With units
Only example

Here is how the Lift given aerodynamic force equation looks like with Values.

Here is how the Lift given aerodynamic force equation looks like with Units.

Here is how the Lift given aerodynamic force equation looks like.

2.926Edit=82.926Edit-80Edit
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Lift given aerodynamic force Solution

Follow our step by step solution on how to calculate Lift given aerodynamic force?

FIRST Step Consider the formula
FL=F-FD
Next Step Substitute values of Variables
FL=82.926N-80N
Next Step Prepare to Evaluate
FL=82.926-80
LAST Step Evaluate
FL=2.926N

Lift given aerodynamic force Formula Elements

Variables
Lift Force
Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow.
Symbol: FL
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Aerodynamic Force
Aerodynamic force is a force exerted on a body by the air in which the body is immersed, and is due to the relative motion between the body and the gas.
Symbol: F
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Drag Force
Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.
Symbol: FD
Measurement: ForceUnit: N
Note: Value can be positive or negative.

Other Formulas to find Lift Force

​Go Lift given Lift Coefficient
FL=CLq
​Go Lift given drag coefficient
FL=CLCDFD
​Go Lift given induced drag
FL=Di3.14qbW2

Other formulas in Lift and Drag Polar category

​Go Drag Coefficient for given parasite drag coefficient
CD=CD,e+(CL2πeoswaldAR)
​Go Drag Coefficient for given zero-lift drag coefficient
CD=CD,0+(CL2πeoswaldAR)
​Go Coefficient of Drag due to lift
CD,i=CL2πeoswaldAR
​Go Parasite Drag Coefficient at zero lift
CD,0=CD-CD,i

How to Evaluate Lift given aerodynamic force?

Lift given aerodynamic force evaluator uses Lift Force = Aerodynamic Force-Drag Force to evaluate the Lift Force, Lift Given Aerodynamic Force is a measure of the upward force exerted on an object, such as an airplane wing, as it moves through the air, calculated by subtracting the drag force from the total aerodynamic force, allowing designers to optimize the shape and performance of aircraft and other objects that interact with air or water. Lift Force is denoted by FL symbol.

How to evaluate Lift given aerodynamic force using this online evaluator? To use this online evaluator for Lift given aerodynamic force, enter Aerodynamic Force (F) & Drag Force (FD) and hit the calculate button.

FAQs on Lift given aerodynamic force

What is the formula to find Lift given aerodynamic force?
The formula of Lift given aerodynamic force is expressed as Lift Force = Aerodynamic Force-Drag Force. Here is an example- -2.926 = 82.926-80.
How to calculate Lift given aerodynamic force?
With Aerodynamic Force (F) & Drag Force (FD) we can find Lift given aerodynamic force using the formula - Lift Force = Aerodynamic Force-Drag Force.
What are the other ways to Calculate Lift Force?
Here are the different ways to Calculate Lift Force-
  • Lift Force=Lift Coefficient*Dynamic PressureOpenImg
  • Lift Force=Lift Coefficient/Drag Coefficient*Drag ForceOpenImg
  • Lift Force=sqrt(Induced Drag*3.14*Dynamic Pressure*Lateral Plane Span^2)OpenImg
Can the Lift given aerodynamic force be negative?
No, the Lift given aerodynamic force, measured in Force cannot be negative.
Which unit is used to measure Lift given aerodynamic force?
Lift given aerodynamic force is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Lift given aerodynamic force can be measured.
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