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## Credits

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## Drag Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
drag_coefficient = 0.00075+(0.000067*Wind Speed at a Height of 10 m)
CD = 0.00075+(0.000067* V10)
This formula uses 1 Variables
Variables Used
Wind Speed at a Height of 10 m - Wind Speed at a Height of 10 m Consideration (Measured in Meter per Second)
STEP 1: Convert Input(s) to Base Unit
Wind Speed at a Height of 10 m: 220 Meter per Second --> 220 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CD = 0.00075+(0.000067* V10) --> 0.00075+(0.000067*220)
Evaluating ... ...
CD = 0.01549
STEP 3: Convert Result to Output's Unit
0.01549 --> No Conversion Required
0.01549 <-- Drag Coefficient
(Calculation completed in 00.016 seconds)

## < 2 Other formulas that you can solve using the same Inputs

Drag Coefficient when Wind Stress is Given
drag_coefficient = Wind Stress/(Density of air*Wind Speed at a Height of 10 m^2) Go
Wind Stress
wind_stress = Drag Coefficient*Density of air*Wind Speed at a Height of 10 m^2 Go

## < 11 Other formulas that calculate the same Output

Drag Coefficient for given zero-lift drag coefficient
drag_coefficient = Zero-lift drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) Go
Drag Coefficient for given parasite drag coefficient
drag_coefficient = Parasite Drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)) Go
Coefficient of drag equation using energy released from blast wave
drag_coefficient = Energy/(0.5*Freestream density*(Freestream Velocity^2)*Diameter ) Go
Drag coefficient of flat plate laminar flow given Schmidt number
drag_coefficient = (2*Convective mass transfer coefficient*(Schmidt Number^0.67))/Free stream velocity Go
Coefficient of Drag for given thrust and weight
drag_coefficient = Thrust of an aircraft*lift coefficient/Weight Go
Coefficient of drag equation with coefficient of normal force
drag_coefficient = coefficient of force*sin(Angle of attack) Go
Coefficient of drag
drag_coefficient = Drag Force/(Dynamic Pressure*Area) Go
Coefficient of Drag for given thrust-to-weight ratio
drag_coefficient = lift coefficient*Thrust-to-weight ratio Go
Coefficient of drag equation with angle of attack
drag_coefficient = 2*(sin(Angle of attack))^3 Go
Drag coefficient of flat plate laminar flow
drag_coefficient = 0.644/(Reynolds Number^0.5) Go
drag coefficient of flat plate laminar flow given friction factor
drag_coefficient = Friction factor/4 Go

### Drag Coefficient Formula

drag_coefficient = 0.00075+(0.000067*Wind Speed at a Height of 10 m)
CD = 0.00075+(0.000067* V10)

## What is Wind Stress?

In Physical Oceanography and Fluid Dynamics, the wind stress is the shear stress exerted by the wind on the surface of large bodies of water – such as oceans, seas, estuaries and lakes. It is the force component parallel to the surface, per unit area, as applied by the wind on the water surface.

## How to Calculate Drag Coefficient?

Drag Coefficient calculator uses drag_coefficient = 0.00075+(0.000067*Wind Speed at a Height of 10 m) to calculate the Drag Coefficient, The Drag Coefficient is approximately equal to the above formulas and is defined as 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 Coefficient and is denoted by CD symbol.

How to calculate Drag Coefficient using this online calculator? To use this online calculator for Drag Coefficient, enter Wind Speed at a Height of 10 m ( V10) and hit the calculate button. Here is how the Drag Coefficient calculation can be explained with given input values -> 0.01549 = 0.00075+(0.000067*220).

### FAQ

What is Drag Coefficient?
The Drag Coefficient is approximately equal to the above formulas and is defined as a 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 = 0.00075+(0.000067* V10) or drag_coefficient = 0.00075+(0.000067*Wind Speed at a Height of 10 m). Wind Speed at a Height of 10 m Consideration.
How to calculate Drag Coefficient?
The Drag Coefficient is approximately equal to the above formulas and is defined as a 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 = 0.00075+(0.000067*Wind Speed at a Height of 10 m). To calculate Drag Coefficient, you need Wind Speed at a Height of 10 m ( V10). With our tool, you need to enter the respective value for Wind Speed at a Height of 10 m 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 Wind Speed at a Height of 10 m. We can use 11 other way(s) to calculate the same, which is/are as follows -
• drag_coefficient = Drag Force/(Dynamic Pressure*Area)
• 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*Thrust-to-weight ratio
• drag_coefficient = Thrust of an aircraft*lift coefficient/Weight
• drag_coefficient = coefficient of force*sin(Angle of attack)
• drag_coefficient = 2*(sin(Angle of attack))^3
• drag_coefficient = Energy/(0.5*Freestream density*(Freestream Velocity^2)*Diameter )
• drag_coefficient = 0.644/(Reynolds Number^0.5)
• drag_coefficient = (2*Convective mass transfer coefficient*(Schmidt Number^0.67))/Free stream velocity
• drag_coefficient = Friction factor/4
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