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Drag coefficient of flat plate laminar flow Formula

GoDrag Coefficient of Flat Plate Laminar Flow using Schmidt Number Formula

GoDrag coefficient of flat plate laminar flow given friction factor Formula

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Drag Coefficient is a dimensionless quantity used to quantify the drag or resistance of an object in a fluid, typically air or water, in laminar flow conditions. Check FAQs

C D = \frac{0.644}{{Re}^{0.5}}

C_D - Drag Coefficient?Re - Reynolds Number?

Drag coefficient of flat plate laminar flow Example

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Here is how the Drag coefficient of flat plate laminar flow equation looks like with Values.

Here is how the Drag coefficient of flat plate laminar flow equation looks like with Units.

Here is how the Drag coefficient of flat plate laminar flow equation looks like.

0.0009 = \frac{0.644}{500000^{0.5}}

0.0009 = \frac{0.644}{500000^{0.5}}

0.0009 = \frac{0.644}{500000^{0.5}}

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Drag coefficient of flat plate laminar flow Solution

Follow our step by step solution on how to calculate Drag coefficient of flat plate laminar flow?

FIRST Step Consider the formula

C D = \frac{0.644}{{Re}^{0.5}}

Next Step Substitute values of Variables

∴

C D = \frac{0.644}{500000^{0.5}}

Next Step Prepare to Evaluate

∴

C D = \frac{0.644}{500000^{0.5}}

Next Step Evaluate

∴

C D = 0.000910753534168273

LAST Step Rounding Answer

∴

C D = 0.0009

Drag coefficient of flat plate laminar flow Formula Elements

Variables

Drag Coefficient

Drag Coefficient is a dimensionless quantity used to quantify the drag or resistance of an object in a fluid, typically air or water, in laminar flow conditions.

Symbol: C_D

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

Reynolds Number

Reynolds Number is a dimensionless value that predicts the nature of fluid flow, either laminar or turbulent, in a pipe or around an object.

Symbol: Re

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Reynolds Number

Other Formulas to find Drag Coefficient

Go Drag Coefficient of Flat Plate Laminar Flow using Schmidt Number

C D = \frac{2 \cdot k L \cdot ({Sc}^{0.67})}{u ∞}

Go Drag coefficient of flat plate laminar flow given friction factor

C D = \frac{f}{4}

Other formulas in Laminar Flow category

Go Mass Transfer Boundary Layer Thickness of Flat Plate in Laminar Flow

δ mx = 𝛿 hx \cdot ({Sc}^{- 0.333})

Go Local Sherwood Number for Flat Plate in Laminar Flow

L sh = 0.332 \cdot ({Re l}^{0.5}) \cdot ({Sc}^{0.333})

Go Sherwood Number for Flat Plate in Laminar Flow

N sh = 0.664 \cdot ({Re}^{0.5}) \cdot ({Sc}^{0.333})

Go Friction factor of flat plate laminar flow

f = \frac{8 \cdot k L \cdot ({Sc}^{0.67})}{u ∞}

How to Evaluate Drag coefficient of flat plate laminar flow?

Drag coefficient of flat plate laminar flow evaluator uses Drag Coefficient = 0.644/(Reynolds Number^0.5) to evaluate the Drag Coefficient, Drag coefficient of flat plate laminar flow formula is defined as a dimensionless quantity that characterizes the drag forces experienced by a flat plate in a laminar flow regime, providing a fundamental parameter in convective mass transfer and fluid dynamics. Drag Coefficient is denoted by C_D symbol.

How to evaluate Drag coefficient of flat plate laminar flow using this online evaluator? To use this online evaluator for Drag coefficient of flat plate laminar flow, enter Reynolds Number (Re) and hit the calculate button.

FAQs on Drag coefficient of flat plate laminar flow

What is the formula to find Drag coefficient of flat plate laminar flow?

The formula of Drag coefficient of flat plate laminar flow is expressed as Drag Coefficient = 0.644/(Reynolds Number^0.5). Here is an example- 0.000911 = 0.644/(500000^0.5).

How to calculate Drag coefficient of flat plate laminar flow?

With Reynolds Number (Re) we can find Drag coefficient of flat plate laminar flow using the formula - Drag Coefficient = 0.644/(Reynolds Number^0.5).

What are the other ways to Calculate Drag Coefficient?

Here are the different ways to Calculate Drag Coefficient-

Drag Coefficient=(2*Convective Mass Transfer Coefficient*(Schmidt Number^0.67))/Free Stream Velocity
Drag Coefficient=Friction Factor/4

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