Drag coefficient new 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: 10 Pascal --> 10 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CD = FD/q --> 80/10
Evaluating ... ...
CD = 8
STEP 3: Convert Result to Output's Unit
8 --> No Conversion Required
FINAL ANSWER
8 <-- Drag Coefficient
(Calculation completed in 00.004 seconds)

Credits

Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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21 Lift and Drag Polar Calculators

Drag Coefficient for given zero-lift drag coefficient
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
Go Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a wing))
Coefficient of Drag due to lift
Go Coefficient of drag due to lift = (Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a wing)
Modern Lift Equation
Go Lift on Airfoil = (Lift Coefficient*Air Density*Aircraft Gross Wing Area*Fluid Velocity^2)/2
Induced drag given span efficiency factor
Go Induced Drag = Drag Coefficient*Density of Material*Velocity^2*Reference Area/2
Lift given induced drag
Go Lift Force = sqrt(Induced Drag*3.14*Dynamic Pressure*Lateral plane span^2)
Induced Drag for Wings having Elliptic Lift Distribution
Go Induced Drag = (Lift Force^2)/(3.14*Dynamic Pressure*Lateral plane span^2)
Coefficient of lift given drag
Go Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force
Coefficient of drag given drag
Go Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
Drag
Go Drag Force = Gross Weight/Lift Coefficient/Drag Coefficient
Lift coefficient given drag coefficient
Go Lift Coefficient = Lift Force/Drag Force*Drag Coefficient
Drag coefficient given lift coefficient
Go Drag Coefficient = Lift Coefficient*Drag Force/Lift Force
Lift given drag coefficient
Go Lift Force = Lift Coefficient/Drag Coefficient*Drag Force
Drag given lift coefficient
Go Drag Force = Lift Force*Drag Coefficient/Lift Coefficient
Parasite Drag Coefficient at zero lift
Go Zero-lift drag coefficient = Drag Coefficient-Coefficient of drag due to lift
Lift given lift coefficient
Go Lift Force = Lift Coefficient*Dynamic Pressure
Drag given drag coefficient
Go Drag Force = Drag Coefficient*Dynamic Pressure
Lift coefficient new
Go Lift Coefficient = Lift Force/Dynamic Pressure
Drag coefficient new
Go Drag Coefficient = Drag Force/Dynamic Pressure
Lift given aerodynamic force
Go Lift Force = Aerodynamic Force-Drag Force
Drag given aerodynamic force
Go Drag Force = Aerodynamic Force-Lift Force

Drag coefficient new Formula

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 new?

Drag coefficient new calculator uses Drag Coefficient = Drag Force/Dynamic Pressure to calculate the Drag Coefficient, The Drag coefficient new formula is defined as dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. Drag Coefficient is denoted by CD symbol.

How to calculate Drag coefficient new using this online calculator? To use this online calculator for Drag coefficient new, enter Drag Force (FD) & Dynamic Pressure (q) and hit the calculate button. Here is how the Drag coefficient new calculation can be explained with given input values -> 8 = 80/10.

FAQ

What is Drag coefficient new?
The Drag coefficient new formula is defined as dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water 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 new?
The Drag coefficient new formula is defined as dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water is calculated using Drag Coefficient = Drag Force/Dynamic Pressure. To calculate Drag coefficient new, 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 4 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
  • Drag Coefficient = Lift Coefficient*Drag Force/Lift Force
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