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November 20, 2018, 02:26 |
combustion efficiency
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#1 |
Member
ARAVIND SRIDHARA
Join Date: Jan 2017
Posts: 32
Rep Power: 9 |
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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November 20, 2018, 10:46 |
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#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,761
Rep Power: 66 |
Don't you have a progress variable in this model? The progress variable helps you distinguish between burnt/unburnt.
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November 21, 2018, 03:28 |
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#3 |
Member
ARAVIND SRIDHARA
Join Date: Jan 2017
Posts: 32
Rep Power: 9 |
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Tags |
flamelet model, hydrogen combustion, non premixed combustion, supersonic.combustion |
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