Drag given drag coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Force = Drag Coefficient*Dynamic Pressure
FD = CD*q
This formula uses 3 Variables
Variables Used
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.
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.
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 Coefficient: 30 --> No Conversion Required
Dynamic Pressure: 2.667 Pascal --> 2.667 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
FD = CD*q --> 30*2.667
Evaluating ... ...
FD = 80.01
STEP 3: Convert Result to Output's Unit
80.01 Newton --> No Conversion Required
FINAL ANSWER
80.01 Newton <-- Drag Force
(Calculation completed in 00.004 seconds)

Credits

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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
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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 given drag coefficient Formula

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

What is drag?

Drag is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.

How to Calculate Drag given drag coefficient?

Drag given drag coefficient calculator uses Drag Force = Drag Coefficient*Dynamic Pressure to calculate the Drag Force, Drag given drag coefficient is a measure of the resistance caused by air or fluid on an object, calculated by multiplying the drag coefficient and dynamic pressure, providing a quantifiable value to understand the forces acting on an object in motion. Drag Force is denoted by FD symbol.

How to calculate Drag given drag coefficient using this online calculator? To use this online calculator for Drag given drag coefficient, enter Drag Coefficient (CD) & Dynamic Pressure (q) and hit the calculate button. Here is how the Drag given drag coefficient calculation can be explained with given input values -> 79.8 = 30*2.667.

FAQ

What is Drag given drag coefficient?
Drag given drag coefficient is a measure of the resistance caused by air or fluid on an object, calculated by multiplying the drag coefficient and dynamic pressure, providing a quantifiable value to understand the forces acting on an object in motion and is represented as FD = CD*q or Drag Force = Drag Coefficient*Dynamic Pressure. 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 & 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 given drag coefficient?
Drag given drag coefficient is a measure of the resistance caused by air or fluid on an object, calculated by multiplying the drag coefficient and dynamic pressure, providing a quantifiable value to understand the forces acting on an object in motion is calculated using Drag Force = Drag Coefficient*Dynamic Pressure. To calculate Drag given drag coefficient, you need Drag Coefficient (CD) & Dynamic Pressure (q). With our tool, you need to enter the respective value for Drag Coefficient & 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 Force?
In this formula, Drag Force uses Drag Coefficient & Dynamic Pressure. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Drag Force = Lift Force*Drag Coefficient/Lift Coefficient
  • Drag Force = Aerodynamic Force-Lift Force
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