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Drag Force on Boundary Layer Flow Plate is the resisting force experienced by an object moving through a fluid. Check FAQs
FD=12CDρfAV2
FD - Drag Force on Boundary Layer Flow Plate?CD - Coefficient of Drag for Boundary Layer Flow?ρf - Fluid Density for Boundary Layer Flow?A - Area of Surface for Boundary Layer Flow?V - Freestream Velocity for Boundary Layer Flow?

Drag Force for Average Drag Coefficient Example

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With units
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Here is how the Drag Force for Average Drag Coefficient equation looks like with Values.

Here is how the Drag Force for Average Drag Coefficient equation looks like with Units.

Here is how the Drag Force for Average Drag Coefficient equation looks like.

0.0298Edit=120.0038Edit890Edit0.79Edit0.15Edit2
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Drag Force for Average Drag Coefficient Solution

Follow our step by step solution on how to calculate Drag Force for Average Drag Coefficient?

FIRST Step Consider the formula
FD=12CDρfAV2
Next Step Substitute values of Variables
FD=120.0038890kg/m³0.790.15m/s2
Next Step Prepare to Evaluate
FD=120.00388900.790.152
Next Step Evaluate
FD=0.02982022875N
LAST Step Rounding Answer
FD=0.0298N

Drag Force for Average Drag Coefficient Formula Elements

Variables
Drag Force on Boundary Layer Flow Plate
Drag Force on Boundary Layer Flow Plate is the resisting force experienced by an object moving through a fluid.
Symbol: FD
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Coefficient of Drag for Boundary Layer Flow
Coefficient of drag for boundary layer flow 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.
Symbol: CD
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Fluid Density for Boundary Layer Flow
Fluid density for boundary layer flow is defined as the mass of fluid per unit volume of the fluid.
Symbol: ρf
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
Area of Surface for Boundary Layer Flow
Area of Surface for boundary layer flow is the surface of the object where the drag force takes place due to the boundary layer.
Symbol: A
Measurement: AreaUnit:
Note: Value should be greater than 0.
Freestream Velocity for Boundary Layer Flow
Freestream velocity for boundary layer flow is the velocity of fluid far upstream of a body, that is before the body has a chance to deflect, slow down the fluid.
Symbol: V
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.

Other Formulas to find Drag Force on Boundary Layer Flow Plate

​Go Drag Force on Plate
FD=0.73bμVRe

Other formulas in Boundary Layer Flow category

​Go Reynold Number at End of Plate
Re=ρfVLμ
​Go Length of Plate for Reynold Number
L=ReμρfV
​Go Velocity of Fluid for Reynold Number
V=ReμρfL
​Go Thickness of Boundary Layer
𝛿=5.48xRe

How to Evaluate Drag Force for Average Drag Coefficient?

Drag Force for Average Drag Coefficient evaluator uses Drag Force on Boundary Layer Flow Plate = 1/2*Coefficient of Drag for Boundary Layer Flow*Fluid Density for Boundary Layer Flow*Area of Surface for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow^2 to evaluate the Drag Force on Boundary Layer Flow Plate, The Drag force for average drag coefficient is known while considering the terms drag coefficient, the density of the fluid, are of the surface or plates, and the freestream velocity. Drag Force on Boundary Layer Flow Plate is denoted by FD symbol.

How to evaluate Drag Force for Average Drag Coefficient using this online evaluator? To use this online evaluator for Drag Force for Average Drag Coefficient, enter Coefficient of Drag for Boundary Layer Flow (CD), Fluid Density for Boundary Layer Flow f), Area of Surface for Boundary Layer Flow (A) & Freestream Velocity for Boundary Layer Flow (V) and hit the calculate button.

FAQs on Drag Force for Average Drag Coefficient

What is the formula to find Drag Force for Average Drag Coefficient?
The formula of Drag Force for Average Drag Coefficient is expressed as Drag Force on Boundary Layer Flow Plate = 1/2*Coefficient of Drag for Boundary Layer Flow*Fluid Density for Boundary Layer Flow*Area of Surface for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow^2. Here is an example- 0.02982 = 1/2*0.00377*890*0.79*0.15^2.
How to calculate Drag Force for Average Drag Coefficient?
With Coefficient of Drag for Boundary Layer Flow (CD), Fluid Density for Boundary Layer Flow f), Area of Surface for Boundary Layer Flow (A) & Freestream Velocity for Boundary Layer Flow (V) we can find Drag Force for Average Drag Coefficient using the formula - Drag Force on Boundary Layer Flow Plate = 1/2*Coefficient of Drag for Boundary Layer Flow*Fluid Density for Boundary Layer Flow*Area of Surface for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow^2.
What are the other ways to Calculate Drag Force on Boundary Layer Flow Plate?
Here are the different ways to Calculate Drag Force on Boundary Layer Flow Plate-
  • Drag Force on Boundary Layer Flow Plate=0.73*Breadth of Plate for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow*sqrt(Reynolds Number for Boundary Layer Flow)OpenImg
Can the Drag Force for Average Drag Coefficient be negative?
No, the Drag Force for Average Drag Coefficient, measured in Force cannot be negative.
Which unit is used to measure Drag Force for Average Drag Coefficient?
Drag Force for Average Drag Coefficient is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Drag Force for Average Drag Coefficient can be measured.
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