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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. Check FAQs
CD=CLFDFL
CD - Drag Coefficient?CL - Lift Coefficient?FD - Drag Force?FL - Lift Force?

Drag coefficient given lift coefficient Example

With values
With units
Only example

Here is how the Drag coefficient given lift coefficient equation looks like with Values.

Here is how the Drag coefficient given lift coefficient equation looks like with Units.

Here is how the Drag coefficient given lift coefficient equation looks like.

30.0752Edit=1.1Edit80Edit2.926Edit
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Drag coefficient given lift coefficient Solution

Follow our step by step solution on how to calculate Drag coefficient given lift coefficient?

FIRST Step Consider the formula
CD=CLFDFL
Next Step Substitute values of Variables
CD=1.180N2.926N
Next Step Prepare to Evaluate
CD=1.1802.926
Next Step Evaluate
CD=30.0751879699248
LAST Step Rounding Answer
CD=30.0752

Drag coefficient given lift coefficient Formula Elements

Variables
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.
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.
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.
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.

Other Formulas to find Drag Coefficient

​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 Drag coefficient given Drag Force
CD=FDq
​Go Coefficient of drag given drag
CD=CLFDW0

Other formulas in Lift and Drag Polar category

​Go Coefficient of Drag due to lift
CD,i=CL2πeoswaldAR
​Go Parasite Drag Coefficient at zero lift
CD,0=CD-CD,i
​Go Modern Lift Equation
L=CLρairSuf22
​Go Lift coefficient given Lift Force
CL=FLq

How to Evaluate Drag coefficient given lift coefficient?

Drag coefficient given lift coefficient evaluator uses Drag Coefficient = Lift Coefficient*Drag Force/Lift Force to evaluate the Drag Coefficient, Drag Coefficient Given Lift Coefficient is a measure of the ratio of drag force to lift force in a fluid dynamics system, providing insight into the relationship between the two forces and enabling calculation of one force when the other is known, this coefficient is crucial in aerodynamics and aerospace engineering, helping to predict and optimize the performance of aircraft, wind turbines, and other systems. Drag Coefficient is denoted by CD symbol.

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

FAQs on Drag coefficient given lift coefficient

What is the formula to find Drag coefficient given lift coefficient?
The formula of Drag coefficient given lift coefficient is expressed as Drag Coefficient = Lift Coefficient*Drag Force/Lift Force. Here is an example- 30.34483 = 1.1*80/2.926.
How to calculate Drag coefficient given lift coefficient?
With Lift Coefficient (CL), Drag Force (FD) & Lift Force (FL) we can find Drag coefficient given lift coefficient using the formula - Drag Coefficient = Lift Coefficient*Drag Force/Lift Force.
What are the other ways to Calculate Drag Coefficient?
Here are the different ways to Calculate Drag Coefficient-
  • Drag Coefficient=Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))OpenImg
  • Drag Coefficient=Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))OpenImg
  • Drag Coefficient=Drag Force/Dynamic PressureOpenImg
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