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Wind Speed at a Height 10 m when Drag Coefficient is Given Calculator

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✖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 Coefficient [CD]
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✖Wind Speed at a Height of 10 m Considerationⓘ Wind Speed at a Height 10 m when Drag Coefficient is Given [ V10]
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Mithila Muthamma PA
Coorg Institute of Technology (CIT), Coorg
Mithila Muthamma PA has created this Calculator and 1000+ more calculators!
Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has verified this Calculator and 1000+ more calculators!

Wind Speed at a Height 10 m when Drag Coefficient is Given Solution

STEP 0: Pre-Calculation Summary
Formula Used
wind_speed_10m_height = (Drag Coefficient-0.00075)/0.000067
V10 = (CD-0.00075)/0.000067
This formula uses 1 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
STEP 1: Convert Input(s) to Base Unit
Drag Coefficient: 100 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
V10 = (CD-0.00075)/0.000067 --> (100-0.00075)/0.000067
Evaluating ... ...
V10 = 1492526.11940299
STEP 3: Convert Result to Output's Unit
1492526.11940299 Meter per Second --> No Conversion Required
FINAL ANSWER
1492526.11940299 Meter per Second <-- Wind Speed at a Height of 10 m
(Calculation completed in 00.016 seconds)
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11 Other formulas that you can solve using the same Inputs

Power required for given aerodynamic coefficients
power = Weight*Freestream Velocity*Drag Coefficient/lift coefficient Go
Weight of aircraft for given coefficients of lift and drag
weight_si = lift coefficient*Thrust of an aircraft/Drag Coefficient Go
Coefficient of Lift for given thrust and weight
lift_coefficient = Weight*Drag Coefficient/Thrust of an aircraft Go
Thrust for given coefficients of lift and drag
thrust_aircraft = Drag Coefficient*Weight/lift coefficient Go
Thrust required for level, unaccelerated flight
thrust_aircraft = Dynamic Pressure*Area*Drag Coefficient Go
Dynamic pressure
dynamic_pressure = Drag Force/(Drag Coefficient*Area) Go
Drag for a level, unaccelerated flight at negligible thrust angle
drag_force = Dynamic Pressure*Area*Drag Coefficient Go
Drag force
drag_force = Drag Coefficient*Dynamic Pressure*Area Go
Parasite Drag Coefficient at zero lift
zero_lift_drag_coefficient = Drag Coefficient-Coefficient of drag due to lift Go
Coefficient of Lift for given thrust-to-weight ratio
lift_coefficient = Drag Coefficient/Thrust-to-weight ratio Go
Thrust-to-weight ratio
thrust_to_weight_ratio = Drag Coefficient/lift coefficient Go

1 Other formulas that calculate the same Output

Wind Speed at a Height 10 m when Wind Stress is Given
wind_speed_10m_height = sqrt(Wind Stress/(Drag Coefficient*Density of air)) Go

Wind Speed at a Height 10 m when Drag Coefficient is Given Formula

wind_speed_10m_height = (Drag Coefficient-0.00075)/0.000067
V10 = (CD-0.00075)/0.000067

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 Wind Speed at a Height 10 m when Drag Coefficient is Given?

Wind Speed at a Height 10 m when Drag Coefficient is Given calculator uses wind_speed_10m_height = (Drag Coefficient-0.00075)/0.000067 to calculate the Wind Speed at a Height of 10 m, Wind Speed at a Height 10 m when Drag Coefficient is Given is defined as the ten-meter wind speed measured ten meters above the top of the datum of consideration. Wind Speed at a Height of 10 m and is denoted by V10 symbol.

How to calculate Wind Speed at a Height 10 m when Drag Coefficient is Given using this online calculator? To use this online calculator for Wind Speed at a Height 10 m when Drag Coefficient is Given, enter Drag Coefficient (CD) and hit the calculate button. Here is how the Wind Speed at a Height 10 m when Drag Coefficient is Given calculation can be explained with given input values -> 1.493E+6 = (100-0.00075)/0.000067.

FAQ

What is Wind Speed at a Height 10 m when Drag Coefficient is Given?
Wind Speed at a Height 10 m when Drag Coefficient is Given is defined as the ten-meter wind speed measured ten meters above the top of the datum of consideration and is represented as V10 = (CD-0.00075)/0.000067 or wind_speed_10m_height = (Drag Coefficient-0.00075)/0.000067. 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.
How to calculate Wind Speed at a Height 10 m when Drag Coefficient is Given?
Wind Speed at a Height 10 m when Drag Coefficient is Given is defined as the ten-meter wind speed measured ten meters above the top of the datum of consideration is calculated using wind_speed_10m_height = (Drag Coefficient-0.00075)/0.000067. To calculate Wind Speed at a Height 10 m when Drag Coefficient is Given, you need Drag Coefficient (CD). With our tool, you need to enter the respective value for Drag Coefficient 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 Wind Speed at a Height of 10 m?
In this formula, Wind Speed at a Height of 10 m uses Drag Coefficient. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • wind_speed_10m_height = sqrt(Wind Stress/(Drag Coefficient*Density of air))
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