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normal shock keep moving reverse inside intake in supersonic 2 ramp compression intak |
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November 27, 2023, 06:47
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normal shock keep moving reverse inside intake in supersonic 2 ramp compression intak
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#1 |
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New Member
Osama Zahid
Join Date: Sep 2023
Posts: 3
Rep Power: 4  |
I am trying to do a 2D analysis of supersonic intake with 2 ramp angles. the normal shock comes back from the diffuser area to the throat but then continues to move forward when I increase the iteration. using steady, DES with k omega SST. can anyone help in this case. pressure at inlet and outlet are provided. flow is of Mach 2.5
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January 3, 2025, 08:16
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#2 |
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Member
Marc Aragó Cebolla
Join Date: Oct 2021
Location: Spain
Posts: 41
Rep Power: 6 |
Hi! Hope you're doing well. I'm working on something similar and thought it would be great to learn more about your situation. Could you share a bit more about details about your case?
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| Tags |
| inlet, intake aerodynamics, normal shock, oblique shock, supersonic |
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