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October 12, 2012, 02:18
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AIR intake for fighter aircraft
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New Member
Rajeev KT
Join Date: Jun 2011
Location: Bangalore
Posts: 6
Rep Power: 14  |
Hi everyone, I am simulating flow through an air intake duct with pressure ratio 0.85, i specified bc's as pressure farfield for flow entering ( 0.1 MACH and pr = 101325) and outlet (-14500pa ) to set back pressure, but i am getting error mesg that flow as been reversed on outlet faces, later i reduced Courant number and tried but residuals are not converging ... so anybody please rectify this problem.
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February 5, 2018, 05:11
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computational modeling of intake
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New Member
amir hossein
Join Date: Nov 2015
Location: Tehran
Posts: 5
Rep Power: 10 |
hi
Due to the complex physics of the flow separation intake, it seems that there is a need for more computational space. Add the duct end to the computational field of intake. |
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