Drag Force Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Force = Drag Coefficient*Dynamic Pressure*Area For Flow
FD = CD*q*A
This formula uses 4 Variables
Variables Used
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
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 is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Area For Flow - (Measured in Square Meter) - Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.
STEP 1: Convert Input(s) to Base Unit
Drag Coefficient: 0.16 --> No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
Area For Flow: 50 Square Meter --> 50 Square Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
FD = CD*q*A --> 0.16*10*50
Evaluating ... ...
FD = 80
STEP 3: Convert Result to Output's Unit
80 Newton --> No Conversion Required
FINAL ANSWER
80 Newton <-- Drag Force
(Calculation completed in 00.004 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
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Verified by Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
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Hypersonic Flow Parameters Calculators

Coefficient of Pressure with Similarity Parameters
​ LaTeX ​ Go Pressure Coefficient = 2*Flow Deflection angle^2*((Specific Heat Ratio+1)/4+sqrt(((Specific Heat Ratio+1)/4)^2+1/Hypersonic Similarity Parameter^2))
Deflection Angle
​ LaTeX ​ Go Deflection Angle = 2/(Specific Heat Ratio-1)*(1/Mach Number ahead of Shock-1/Mach Number Behind Shock)
Coefficient of Drag
​ LaTeX ​ Go Drag Coefficient = Drag Force/(Dynamic Pressure*Area For Flow)
Axial Force Coefficient
​ LaTeX ​ Go Coefficient of Force = Force/(Dynamic Pressure*Area For Flow)

Drag Force Formula

​LaTeX ​Go
Drag Force = Drag Coefficient*Dynamic Pressure*Area For Flow
FD = CD*q*A

What is drag force?

n fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) 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 surfaces) or a fluid and a solid surface

How to Calculate Drag Force?

Drag Force calculator uses Drag Force = Drag Coefficient*Dynamic Pressure*Area For Flow to calculate the Drag Force, Drag Force formula is defined as a measure of the resistance to the motion of an object through a fluid, typically air or water, resulting from the interaction between the object and the fluid, and is a critical parameter in the study of hypersonic flow and aerodynamics. Drag Force is denoted by FD symbol.

How to calculate Drag Force using this online calculator? To use this online calculator for Drag Force, enter Drag Coefficient (CD), Dynamic Pressure (q) & Area For Flow (A) and hit the calculate button. Here is how the Drag Force calculation can be explained with given input values -> 15000 = 0.16*10*50.

FAQ

What is Drag Force?
Drag Force formula is defined as a measure of the resistance to the motion of an object through a fluid, typically air or water, resulting from the interaction between the object and the fluid, and is a critical parameter in the study of hypersonic flow and aerodynamics and is represented as FD = CD*q*A or Drag Force = Drag Coefficient*Dynamic Pressure*Area For Flow. 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 is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid & Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.
How to calculate Drag Force?
Drag Force formula is defined as a measure of the resistance to the motion of an object through a fluid, typically air or water, resulting from the interaction between the object and the fluid, and is a critical parameter in the study of hypersonic flow and aerodynamics is calculated using Drag Force = Drag Coefficient*Dynamic Pressure*Area For Flow. To calculate Drag Force, you need Drag Coefficient (CD), Dynamic Pressure (q) & Area For Flow (A). With our tool, you need to enter the respective value for Drag Coefficient, Dynamic Pressure & Area For Flow and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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