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July 31, 2018, 12:15 |
Valveless Pulsejet
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#1 |
New Member
Andreia
Join Date: Jun 2018
Posts: 13
Rep Power: 7 |
Hello I'm trying to simulate a valveless pulsejet using ansys fluent. My model is an advanced focussed wave type. I am using transient model, energy equation on, for the viscosityK-epsilon SST model , radiation: P1 and for the species partially premixed combustion . For BCs I have only one pressure inlet (here is a big part of my doubt) with gauss pressure 0 and mean mixture fraction 0.064 (I'm using a stoichiometric propane-air mixture). For the outlet I have pressure outlet also with gauss pressure 0 and progress variable 1. The walls are defined as convective.
My problem is that when I start running I can not get combustion, the fuel does not flow into the combustion chamber. What should I do? |
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August 7, 2018, 15:42 |
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#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
Rep Power: 66 |
Does it make sense for the inlet and outlet to be at the same pressure for this problem? What drives the flow?
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August 8, 2018, 10:51 |
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#3 |
New Member
Andreia
Join Date: Jun 2018
Posts: 13
Rep Power: 7 |
Yes you right, i've change the inlet pressure to 10.
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