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Search: Posts Made By: quiqui
Forum: FLUENT June 18, 2013, 12:28
Replies: 21
Views: 4,022
Posted By quiqui
Which means you did not import the profile as the...

Which means you did not import the profile as the total pressure @ pressure inlet, you use a specific number? right?

I used to run the case @ 70 psi, it run well, but once I imported the...
Forum: FLUENT June 18, 2013, 11:12
Replies: 21
Views: 4,022
Posted By quiqui
hi I saved the mesh file and profile in draft @...

hi
I saved the mesh file and profile in draft @ a gmail account

user: fluent111
password: 1234506789

thanks
Forum: FLUENT June 18, 2013, 10:35
Replies: 21
Views: 4,022
Posted By quiqui
I revised the o psi to the static pressure and...

I revised the o psi to the static pressure and tried, it gave the same error when compute from inlet.
still cannot run the case
Forum: FLUENT June 18, 2013, 10:31
Replies: 21
Views: 4,022
Posted By quiqui
yes, I notice this. I will remove the o points...

yes, I notice this. I will remove the o points and try.
Forum: FLUENT June 18, 2013, 10:21
Replies: 21
Views: 4,022
Posted By quiqui
to capture the shock with separation, the mesh is...

to capture the shock with separation, the mesh is very fine, so I only posted the geometry.
Forum: FLUENT June 18, 2013, 10:18
Replies: 21
Views: 4,022
Posted By quiqui
in supersonic case, operating pressure is 0. 70...

in supersonic case, operating pressure is 0.
70 psi is the total pressure.
Forum: FLUENT June 18, 2013, 10:16
Replies: 21
Views: 4,022
Posted By quiqui
yes, there is 0 psi, which is @ the wall. I...

yes, there is 0 psi, which is @ the wall.

I tried running without profile, it gave the experimental trend, but after some running, I import the profile, It gave me the error immediately.
Forum: FLUENT June 18, 2013, 10:13
Replies: 21
Views: 4,022
Posted By quiqui
If I initialized the x velocity with 300 m/s, the...

If I initialized the x velocity with 300 m/s, the computing velocity result cannot reach the actual velocity.
In experiments, with total pressure @ 70 psi, total temperature 300k, static pressure...
Forum: FLUENT June 18, 2013, 10:07
Replies: 21
Views: 4,022
Posted By quiqui
yes, supersonic flow with Mach number 1.9 @...

yes, supersonic flow with Mach number 1.9 @ total pressure 70 psi, and total temperature 300 K.
Forum: FLUENT June 18, 2013, 09:46
Replies: 21
Views: 4,022
Posted By quiqui
attached is the sketch and profile data.

attached is the sketch and profile data.
Forum: FLUENT June 18, 2013, 09:37
Replies: 21
Views: 4,022
Posted By quiqui
no, I only have one inlet, one outlet.

no, I only have one inlet, one outlet.
Forum: FLUENT June 17, 2013, 14:57
Replies: 21
Views: 4,022
Posted By quiqui
help with boundary profile in pressure inlet

Hi
I built a 2-d model, using pressure inlet and pressure outlet.
I have the experimental inlet boundary total pressure data(attached). I used these data for a boundary profile.
...
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