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Old   February 4, 2004, 10:45
Default ramjet inlet
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AE
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hi,

Did anybody ever model ramjet inlet using Fluent?

Regards

AE
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Old   February 5, 2004, 05:12
Default Re: ramjet inlet
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Nandu
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HI,

are you trying to model the entire ramjet including the combustion physics? or simply the inlet with the shock cone?

nandu
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Old   February 5, 2004, 09:08
Default Re: ramjet inlet
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AE
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Hi,

I am trying to model only the inlet. The flow is a bit complicated from 3 Ma to 0.3 Ma with oblique shocks and normal shocks. Some are as shock trains.

Fluent is the market leader especially in Aero industry, but how good is it in solving such wide-range flows?

Would you share your experience?

Best AE

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Old   February 5, 2004, 09:26
Default Re: ramjet inlet
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Nandu
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Hi,

Simply the inlet should not be a problem using the coupled solver fo fluent. We have had very good success in modelling a wide range of supersonic flow field ranging from Mach 1.5 to M = 5. We'd be glad to help out in any way we can. u can reach me directly at my email (nmenon@mech.wits.ac.za)

nandu

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Old   February 5, 2004, 11:35
Default Re: ramjet inlet
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AE
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Cheers!!

Thanks a lot..

AE
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