Transform flow around a cylinder to cartesian

The relation is pretty straightforward and simple, just remember the definitions of the unit vectors in both coordinate systems.In summary, the conversation discusses transforming a flow field described in cylindrical coordinates into cartesian coordinates. The equations for the link between the two coordinate systems are provided, and the process of transforming the velocity components for u_r and u_{\theta} is shown. The conversation ends with the question of how to separate the x and y parts of u_{\theta} and u_r to find the velocities in cartesian coordinates, and the suggestion to find the relation between the two coordinate systems to solve this problem.
  • #1
MichielM
23
0

Homework Statement


A flow field is considered to be steady two-dimensional and can be described by the following
velocity components in the xy- or r[tex]\theta[/tex]-plane at the front half of the cylinder:
[tex]
u_r=V\cos\theta\left(1-\frac{a^2}{r^2}\right)
[/tex]
[tex]
u_{\theta}=-V\sin\theta\left(1+\frac{a^2}{r^2}\right)
[/tex]

Question: Transform this system from cylindrical coordinates into cartesian coordinates and give [tex]u_x[/tex], [tex]u_y[/tex] and [tex]u_z[/tex]

Homework Equations


The link between cartesian and cylindrical coordinates is:
[tex] x = x [/tex]
[tex]y = r \cos \theta[/tex]
[tex]z = r \sin \theta[/tex]

or the other way around:
[tex] x = x [/tex]
[tex]r^2 = x^2+y^2[/tex]
[tex]\theta =tan^{-1}(y/x)[/tex]

The Attempt at a Solution


For [tex]u_r[/tex] I take 1 term r outside the brackets and then transform to get:
[tex]
u_r=V y \left(\frac{1}{x^2+y^2}-\frac{a^2}{\left(x^2+y^2\right)^3}\right)
[/tex]
And similarly for [tex]u_{\theta}[/tex] I get:
[tex]
u_{\theta}=-V x \left(\frac{1}{x^2+y^2}+\frac{a^2}{\left(x^2+y^2\right)^3}\right)
[/tex]

This is where I get stuck, because I don't know how to separate the x and y parts of [tex]u_{\theta}[/tex] and [tex]u_{r}[/tex] to find the velocities in cartesian coordinates. Does anyone have any hints?!
 
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  • #2
You want to find an expression of some vector u in Cartesian coordinates. In other words you're interested in [itex]\mathbf{u}=u_x \mathbf{\hat{x}}+u_y \mathbf{\hat{y}}+u_z \mathbf{\hat{z}}[/itex]. However you have the vector u as [itex]\mathbf{u}=u_x \mathbf{\hat{x}}+u_r \mathbf{\hat{r}}+u_\theta \mathbf{\hat{\theta}}[/itex]. To get your answer you need to find a relation between the Cartesian and cylindrical unit vectors. You can find this relation in your book or derive it yourself.
 

FAQ: Transform flow around a cylinder to cartesian

1. What is a transform flow around a cylinder?

Transform flow around a cylinder refers to the mathematical process of converting the flow of fluids around a cylindrical object into a Cartesian coordinate system. This transformation allows for easier analysis and visualization of the flow pattern.

2. Why is it important to transform flow around a cylinder to cartesian?

Transforming flow around a cylinder to cartesian coordinates allows for a more simplified and accurate representation of the flow pattern. It also makes it easier to compare and analyze the flow with other types of fluid flow.

3. How is the transform flow around a cylinder to cartesian done?

The transformation is done using mathematical equations and formulas that convert the cylindrical coordinates (r, θ, z) into cartesian coordinates (x, y, z). This process is typically done using computer software or programming languages.

4. What factors can affect the transform flow around a cylinder to cartesian?

The accuracy of the transformation can be affected by various factors such as the shape and size of the cylinder, the density and viscosity of the fluid, and the speed and direction of the flow. Other factors such as turbulence and boundary conditions can also play a role.

5. What are some practical applications of transforming flow around a cylinder to cartesian?

Transforming flow around a cylinder to cartesian coordinates is commonly used in engineering, aerodynamics, and fluid mechanics. It can help in the design and analysis of various structures such as aircraft wings, wind turbines, and pipes, as well as in predicting the behavior of fluids in different scenarios.

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