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Flow analysis in a Convergent-Divergent Nozzle (URGENT!) |
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June 16, 2009, 04:00
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Problem was Solved.
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#1 |
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Aerospace Engineer
Join Date: Jun 2009
Posts: 6
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Problem was solved.
Last edited by hasan_hzl; June 26, 2009 at 04:03. |
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June 17, 2009, 11:51
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#2 |
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Aerospace Engineer
Join Date: Jun 2009
Posts: 6
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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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June 30, 2009, 00:46
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floating point
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#3 |
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New Member
Sudharshani
Join Date: Jun 2009
Location: Melbourne,Australia
Posts: 16
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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? sudhar |
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