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alireza-kh September 26, 2010 01:40
supersonic wind tunnel
 
2 Attachment(s)
hi everybody

I try to simulate a supersonic wind tunnel. (see attached file). I use pressure inlet-outlet BC. my problem is 2D and inviscid. method is implicit and steady. I use courant number about 0.5 but residual don't decrease. a sample of residual is attached. please help me.

JohnPeclet June 26, 2015 09:28
Quote:
Originally Posted by alireza-kh (Post 276651)
hi everybody

I try to simulate a supersonic wind tunnel. (see attached file). I use pressure inlet-outlet BC. my problem is 2D and inviscid. method is implicit and steady. I use courant number about 0.5 but residual don't decrease. a sample of residual is attached. please help me.
Hi

Have you had any progress with it? Do you perhaps have the Pressure Contours? If so, would you mind posting it?

aminz April 11, 2024 17:23
Quote:
Originally Posted by alireza-kh (Post 276651)
hi everybody

I try to simulate a supersonic wind tunnel. (see attached file). I use pressure inlet-outlet BC. my problem is 2D and inviscid. method is implicit and steady. I use courant number about 0.5 but residual don't decrease. a sample of residual is attached. please help me.
I faced the same issue and I’m having trouble setting up BCS for this. Can you help me out

aeroshiva7 April 12, 2024 06:12
Hi i can help you let me know if it is paid task, connect me at aeroshivakumar(at)gmaildotcom


QUOTE=aminz;867620]I faced the same issue and I’m having trouble setting up BCS for this. Can you help me out[/QUOTE]


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