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Old   November 20, 2018, 02:26
Default combustion efficiency
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ARAVIND SRIDHARA
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Hii,
I am modeling a a flow involving supersonic flows with the effects of combustion. my fuel is hydrogen and air is oxidizer. i use laminar flamelet model to model reacting flows. the calculation is complete. i want to find out combustion efficiency which is (1-mass flow rate of hydrogen/ unburnt hydrogen mass flow rate). I simply get the mass flow rate of hydrogen burnt / consumed by integrating (density*Yhydrogen*V*A) (Y_hydrogen at a given streamwise location) along the leangth of the combustor. But how do i find out the unburnt hydrogen mass fraction present along the combustor length.

I thank readers for their valuable suggestions.
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Old   November 20, 2018, 10:46
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Don't you have a progress variable in this model? The progress variable helps you distinguish between burnt/unburnt.
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Old   November 21, 2018, 03:28
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Quote:
Originally Posted by LuckyTran View Post
Don't you have a progress variable in this model? The progress variable helps you distinguish between burnt/unburnt.
i use non-premixed laminar steady flamelet model. I dont know about progress variable, and how to set values for it
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flamelet model, hydrogen combustion, non premixed combustion, supersonic.combustion


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