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Flow analysis in a Convergent-Divergent Nozzle (URGENT!)

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Old   June 16, 2009, 05:00
Exclamation Problem was Solved.
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Problem was solved.

Last edited by hasan_hzl; June 26, 2009 at 05:03.
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Old   June 17, 2009, 12:51
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I tried to solve it give an error of "floating point". I think it is because of big pressure difference btw inlet and outlet. Now what do I have to do? Please help me
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Old   June 30, 2009, 01:46
Default floating point
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what is a floating point point?
which software are u using as i am also doing the same problem(supersonic CD nozzle) using ANSYS CFX...just started my project.
how did u designed ur nozzle shape? is it through parameric modeling of a function or do u have fixed data set?
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