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September 26, 2017, 01:49
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Reacting Supersonic Flow
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New Member
Ahmad Ijaz
Join Date: Jun 2017
Location: Islamabad, Pakistan
Posts: 13
Rep Power: 10  |
Hi
I am trying to model combustion reaction of UDMH+N2O4 in supersonic condition flow. I am actually trying to reproduce the results of the paper "Numerical Simulation of Pintle Variable Thrust Rocket Engine". I am confused with the outlet boundary condition. Can anyone elaborate me this line: "Export boundary was dealt with supersonic speed, parameters were obtained according to external value-inserting method of neighboring upstream parameters." |
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September 27, 2017, 07:46
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#2 |
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New Member
Ahmad Ijaz
Join Date: Jun 2017
Location: Islamabad, Pakistan
Posts: 13
Rep Power: 10 |
Can anyone only elaborate me this line, I will be very grateful:
"Export boundary was dealt with supersonic speed, parameters were obtained according to external value-inserting method of neighboring upstream parameters." Thanks in Advance ! |
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