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The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. Check FAQs
CL=FLFDCD
CL - Lift Coefficient?FL - Lift Force?FD - Drag Force?CD - Drag Coefficient?

Lift coefficient given drag coefficient Example

With values
With units
Only example

Here is how the Lift coefficient given drag coefficient equation looks like with Values.

Here is how the Lift coefficient given drag coefficient equation looks like with Units.

Here is how the Lift coefficient given drag coefficient equation looks like.

1.0972Edit=2.926Edit80Edit30Edit
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Lift coefficient given drag coefficient Solution

Follow our step by step solution on how to calculate Lift coefficient given drag coefficient?

FIRST Step Consider the formula
CL=FLFDCD
Next Step Substitute values of Variables
CL=2.926N80N30
Next Step Prepare to Evaluate
CL=2.9268030
Next Step Evaluate
CL=1.09725
LAST Step Rounding Answer
CL=1.0972

Lift coefficient given drag coefficient Formula Elements

Variables
Lift Coefficient
The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Symbol: CL
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
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.
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.
Drag Coefficient
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Symbol: CD
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.

Other Formulas to find Lift Coefficient

​Go Lift coefficient given Lift Force
CL=FLq
​Go Coefficient of lift given drag
CL=W0CDFD

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 coefficient given drag coefficient?

Lift coefficient given drag coefficient evaluator uses Lift Coefficient = Lift Force/Drag Force*Drag Coefficient to evaluate the Lift Coefficient, Lift Coefficient Given Drag Coefficient is a dimensionless quantity that represents the ratio of lift force to drag force in an aerodynamic system, providing a measure of the efficiency of an airfoil or wing design in producing lift while minimizing drag, it is a crucial parameter in aerodynamics, used to evaluate and optimize the performance of aircraft, wind turbines, and other aerodynamic systems. Lift Coefficient is denoted by CL symbol.

How to evaluate Lift coefficient given drag coefficient using this online evaluator? To use this online evaluator for Lift coefficient given drag coefficient, enter Lift Force (FL), Drag Force (FD) & Drag Coefficient (CD) and hit the calculate button.

FAQs on Lift coefficient given drag coefficient

What is the formula to find Lift coefficient given drag coefficient?
The formula of Lift coefficient given drag coefficient is expressed as Lift Coefficient = Lift Force/Drag Force*Drag Coefficient. Here is an example- 1.0875 = 2.926/80*30.
How to calculate Lift coefficient given drag coefficient?
With Lift Force (FL), Drag Force (FD) & Drag Coefficient (CD) we can find Lift coefficient given drag coefficient using the formula - Lift Coefficient = Lift Force/Drag Force*Drag Coefficient.
What are the other ways to Calculate Lift Coefficient?
Here are the different ways to Calculate Lift Coefficient-
  • Lift Coefficient=Lift Force/Dynamic PressureOpenImg
  • Lift Coefficient=(Gross Weight*Drag Coefficient)/Drag ForceOpenImg
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