Drag coefficient of flat plate in combined laminar turbulent flow Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Coefficient = 0.0571/(Reynolds Number^0.2)
CD = 0.0571/(Re^0.2)
This formula uses 2 Variables
Variables Used
Drag Coefficient - Drag Coefficient is a dimensionless quantity used to quantify the drag force experienced by an object in laminar and turbulent fluid flows.
Reynolds Number - Reynolds Number is a dimensionless value that predicts the nature of fluid flow, whether it will be laminar or turbulent, in a given flow situation.
STEP 1: Convert Input(s) to Base Unit
Reynolds Number: 500000 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CD = 0.0571/(Re^0.2) --> 0.0571/(500000^0.2)
Evaluating ... ...
CD = 0.00413849187959964
STEP 3: Convert Result to Output's Unit
0.00413849187959964 --> No Conversion Required
FINAL ANSWER
0.00413849187959964 0.004138 <-- Drag Coefficient
(Calculation completed in 00.004 seconds)

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Shri Madhwa Vadiraja Institute of Technology and Management (SMVITM), Udupi
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Drag coefficient of flat plate in combined laminar turbulent flow
​ LaTeX ​ Go Drag Coefficient = 0.0571/(Reynolds Number^0.2)

Drag coefficient of flat plate in combined laminar turbulent flow Formula

​LaTeX ​Go
Drag Coefficient = 0.0571/(Reynolds Number^0.2)
CD = 0.0571/(Re^0.2)

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 in combined laminar turbulent flow?

Drag coefficient of flat plate in combined laminar turbulent flow calculator uses Drag Coefficient = 0.0571/(Reynolds Number^0.2) to calculate the Drag Coefficient, Drag coefficient of flat plate in combined laminar turbulent flow formula is defined as a dimensionless quantity that characterizes the drag properties of a flat plate in a fluid flow, combining both laminar and turbulent flow regimes, and is used to predict the drag force experienced by the plate. Drag Coefficient is denoted by CD symbol.

How to calculate Drag coefficient of flat plate in combined laminar turbulent flow using this online calculator? To use this online calculator for Drag coefficient of flat plate in combined laminar turbulent flow, enter Reynolds Number (Re) and hit the calculate button. Here is how the Drag coefficient of flat plate in combined laminar turbulent flow calculation can be explained with given input values -> 0.004138 = 0.0571/(500000^0.2).

FAQ

What is Drag coefficient of flat plate in combined laminar turbulent flow?
Drag coefficient of flat plate in combined laminar turbulent flow formula is defined as a dimensionless quantity that characterizes the drag properties of a flat plate in a fluid flow, combining both laminar and turbulent flow regimes, and is used to predict the drag force experienced by the plate and is represented as CD = 0.0571/(Re^0.2) or Drag Coefficient = 0.0571/(Reynolds Number^0.2). Reynolds Number is a dimensionless value that predicts the nature of fluid flow, whether it will be laminar or turbulent, in a given flow situation.
How to calculate Drag coefficient of flat plate in combined laminar turbulent flow?
Drag coefficient of flat plate in combined laminar turbulent flow formula is defined as a dimensionless quantity that characterizes the drag properties of a flat plate in a fluid flow, combining both laminar and turbulent flow regimes, and is used to predict the drag force experienced by the plate is calculated using Drag Coefficient = 0.0571/(Reynolds Number^0.2). To calculate Drag coefficient of flat plate in combined laminar turbulent 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.
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