Let’s see if this works:
![\frac{V}{V^*} = M^* = M\left[\frac{\gamma+1}{2\left(1+\frac{\gamma-1}{2}M^2\right)}\right]^{\frac{1}{2}}](http://www.tdkpropulsion.com/wp-content/cache/tex_1abb80350bda684d3d157f3d37c44422.png)
Well, isn’t that lovely!
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May 10th, 2008 at 11:45 pm
Let’s also have a look-see if it works in a comment. If so, you’ll find yourself with the equations for stagnation velocity and absolute static pressure in a flow with mass addition normal to the main stream:
June 17th, 2008 at 12:56 am
http://www.tdkpropulsion.com/wp-content/cache/tex_428fb0b81339f4a92596ee44c2c96591.png
\frac{p}{p^*} = \frac{\gamma + 1}{1+\gamma M^2} well done
anyway looking forward to seeing some more motors
June 23rd, 2008 at 11:47 am
Close – you need an extra $ before the usual LaTeX declaration statement, so the syntax is:
$ $ LaTeX $ $
(without the spaces). To activate math mode, add an extra ! after the initial two $s. The full plugin documentation is at http://wordpress.org/extend/plugins/latex/
Anyways, once I get back from Rome I have some things to update with. It’s a bit dry on rocket news here, though.