MichielM
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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\theta-plane at the front half of the cylinder:
<br /> u_r=V\cos\theta\left(1-\frac{a^2}{r^2}\right)<br />
<br /> u_{\theta}=-V\sin\theta\left(1+\frac{a^2}{r^2}\right)<br />
Question: Transform this system from cylindrical coordinates into cartesian coordinates and give u_x, u_y and u_z
Homework Equations
The link between cartesian and cylindrical coordinates is:
x = x
y = r \cos \theta
z = r \sin \theta
or the other way around:
x = x
r^2 = x^2+y^2
\theta =tan^{-1}(y/x)
The Attempt at a Solution
For u_r I take 1 term r outside the brackets and then transform to get:
<br /> u_r=V y \left(\frac{1}{x^2+y^2}-\frac{a^2}{\left(x^2+y^2\right)^3}\right)<br />
And similarly for u_{\theta} I get:
<br /> u_{\theta}=-V x \left(\frac{1}{x^2+y^2}+\frac{a^2}{\left(x^2+y^2\right)^3}\right)<br />
This is where I get stuck, because I don't know how to separate the x and y parts of u_{\theta} and u_{r} to find the velocities in cartesian coordinates. Does anyone have any hints?!
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