Drag coefficient given Drag Force Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Coefficient = Drag Force/Dynamic Pressure
CD = FD/q
This formula uses 3 Variables
Variables Used
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.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.
Dynamic Pressure - (Measured in Pascal) - Dynamic pressure, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.
STEP 1: Convert Input(s) to Base Unit
Drag Force: 80 Newton --> 80 Newton No Conversion Required
Dynamic Pressure: 2.667 Pascal --> 2.667 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CD = FD/q --> 80/2.667
Evaluating ... ...
CD = 29.9962504686914
STEP 3: Convert Result to Output's Unit
29.9962504686914 --> No Conversion Required
FINAL ANSWER
29.9962504686914 29.99625 <-- Drag Coefficient
(Calculation completed in 00.004 seconds)

Credits

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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
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Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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Lift and Drag Polar Calculators

Drag Coefficient for given zero-lift drag coefficient
​ LaTeX ​ Go Drag Coefficient = Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
Drag Coefficient for given parasite drag coefficient
​ LaTeX ​ Go Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
Coefficient of Drag due to lift
​ LaTeX ​ Go Coefficient of Drag due to Lift = (Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing)
Parasite Drag Coefficient at zero lift
​ LaTeX ​ Go Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift

Drag coefficient given Drag Force Formula

​LaTeX ​Go
Drag Coefficient = Drag Force/Dynamic Pressure
CD = FD/q

What is drag force?

In fluid dynamics, drag is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid. This can exist between two fluid layers or between a fluid and a solid surface.

How to Calculate Drag coefficient given Drag Force?

Drag coefficient given Drag Force calculator uses Drag Coefficient = Drag Force/Dynamic Pressure to calculate the Drag Coefficient, Drag coefficient given Drag Force represents a dimensionless quantity that represents the resistance to motion of an object through a fluid, such as air or water, and is calculated as the ratio of the drag force to the dynamic pressure. Drag Coefficient is denoted by CD symbol.

How to calculate Drag coefficient given Drag Force using this online calculator? To use this online calculator for Drag coefficient given Drag Force, enter Drag Force (FD) & Dynamic Pressure (q) and hit the calculate button. Here is how the Drag coefficient given Drag Force calculation can be explained with given input values -> 30.07519 = 80/2.667.

FAQ

What is Drag coefficient given Drag Force?
Drag coefficient given Drag Force represents a dimensionless quantity that represents the resistance to motion of an object through a fluid, such as air or water, and is calculated as the ratio of the drag force to the dynamic pressure and is represented as CD = FD/q or Drag Coefficient = Drag Force/Dynamic Pressure. Drag Force is the resisting force experienced by an object moving through a fluid ,such as air & Dynamic pressure, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.
How to calculate Drag coefficient given Drag Force?
Drag coefficient given Drag Force represents a dimensionless quantity that represents the resistance to motion of an object through a fluid, such as air or water, and is calculated as the ratio of the drag force to the dynamic pressure is calculated using Drag Coefficient = Drag Force/Dynamic Pressure. To calculate Drag coefficient given Drag Force, you need Drag Force (FD) & Dynamic Pressure (q). With our tool, you need to enter the respective value for Drag Force & Dynamic Pressure and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Drag Coefficient?
In this formula, Drag Coefficient uses Drag Force & Dynamic Pressure. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
  • Drag Coefficient = Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
  • Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
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