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October 5, 2006, 21:52 |
Hypersonic flow capabilities
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#1 |
Guest
Posts: n/a
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Hi,
Can FLUENT handle hypersonic flows, i.e. say a velocity of Mach 20 - 30, which may be experienced by space shuttles during reentry? If not, is there any other software in the market which can, or is specifically suited to do so? Thank you. |
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October 5, 2006, 22:03 |
Re: Hypersonic flow capabilities
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#2 |
Guest
Posts: n/a
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If you write the proper UDF functions to handle the effects of dissociation on fluid properties, the answer is Yes
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October 6, 2006, 10:10 |
Re: Hypersonic flow capabilities
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#3 |
Guest
Posts: n/a
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Fluent's density based solver(Coupled sover) does not have any limitation on Mach number. Using UDF for air chemistry to account for dissociation of air, you can get better results.
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June 4, 2014, 15:02 |
UDF to Model Finite Rate Chemistry
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#4 |
Member
Mike
Join Date: Jun 2012
Posts: 58
Rep Power: 14 |
Hi,
I am simulating hypersonic flow over a sphere. I would like to use Fluent's Finite Rate Chemistry Model. I have a reaction file which I used on CFD++ software. However, I realized that I need to re-format this UDF to use in Fluent. Does anyone have advice on the structure of this UDF? If anyone has an example UDF with the correct format for the reactions, I would be greatful! Thanks |
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