Drag coefficient of flat plate laminar flow Calculator

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

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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.ⓘ Drag coefficient of flat plate laminar flow [C_D]

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Drag coefficient of flat plate laminar flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Coefficient = 0.644/(Reynolds Number^0.5)
C_D = 0.644/(Re^0.5)
This formula uses 2 Variables

Variables Used

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.
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.

STEP 1: Convert Input(s) to Base Unit

Reynolds Number: 500000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D = 0.644/(Re^0.5) --> 0.644/(500000^0.5)

Evaluating ... ...

C_D = 0.000910753534168273

STEP 3: Convert Result to Output's Unit

0.000910753534168273 --> No Conversion Required

FINAL ANSWER

0.000910753534168273 ≈ 0.000911 <-- Drag Coefficient

(Calculation completed in 00.020 seconds)

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Created by Nishan Poojary

Shri Madhwa Vadiraja Institute of Technology and Management (SMVITM), Udupi

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Verified by Sagar S Kulkarni

Dayananda Sagar College of Engineering (DSCE), Bengaluru

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< Laminar Flow Calculators

Mass Transfer Boundary Layer Thickness of Flat Plate in Laminar Flow

LaTeX Go Mass Transfer Boundary Layer Thickness at x = Hydrodynamic Boundary Layer Thickness*(Schmidt Number^(-0.333))

Local Sherwood Number for Flat Plate in Laminar Flow

LaTeX Go Local Sherwood Number = 0.332*(Local Reynolds Number^0.5)*(Schmidt Number^0.333)

Sherwood Number for Flat Plate in Laminar Flow

LaTeX Go Average Sherwood Number = 0.664*(Reynolds Number^0.5)*(Schmidt Number^0.333)

Drag coefficient of flat plate laminar flow

LaTeX Go Drag Coefficient = 0.644/(Reynolds Number^0.5)

Drag coefficient of flat plate laminar flow Formula

LaTeX Go

Drag Coefficient = 0.644/(Reynolds Number^0.5)
C_D = 0.644/(Re^0.5)

What is Drag Coefficient?

The drag coefficient is a dimensionless number that quantifies the drag or resistance experienced by an object moving through a fluid, such as air or water. It is defined as the ratio of the drag force acting on the object to the product of the fluid density, the object's velocity, and its reference area (typically the cross-sectional area). The drag coefficient depends on factors such as the object's shape, surface roughness, and the flow conditions (laminar or turbulent). It is commonly used in engineering and aerodynamics to predict the drag force on vehicles, aircraft, and other objects, helping to optimize their design for improved performance and efficiency.

How to Calculate Drag coefficient of flat plate laminar flow?

Drag coefficient of flat plate laminar flow calculator uses Drag Coefficient = 0.644/(Reynolds Number^0.5) to calculate 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 calculate Drag coefficient of flat plate laminar flow using this online calculator? To use this online calculator for Drag coefficient of flat plate laminar flow, enter Reynolds Number (Re) and hit the calculate button. Here is how the Drag coefficient of flat plate laminar flow calculation can be explained with given input values -> 0.000911 = 0.644/(500000^0.5).

FAQ

What is Drag coefficient of flat plate laminar flow?

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 and is represented as C_D = 0.644/(Re^0.5) or Drag Coefficient = 0.644/(Reynolds Number^0.5). Reynolds Number is a dimensionless value that predicts the nature of fluid flow, either laminar or turbulent, in a pipe or around an object.

How to calculate Drag coefficient of flat plate laminar flow?

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 is calculated using Drag Coefficient = 0.644/(Reynolds Number^0.5). To calculate Drag coefficient of flat plate laminar flow, you need Reynolds Number (Re). With our tool, you need to enter the respective value for Reynolds Number 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 Reynolds Number. We can use 2 other way(s) to calculate the same, which is/are as follows -

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

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