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Hi
I have downloaded the solver and have had a look at the features available in the code. From the 2014 AIAA paper, I understand that a well-resolved boundary layer over a flat plate could be genera…
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On my machine, the supersonic flow example takes around 60s to run. @jb803: is there any way to speed this up? Otherwise running the test suite becomes tedious.
rjw57 updated
8 years ago
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Q1:
For viscous simulation, the size of input mesh file must be in meters, is it?
Q2:
There are no parameters about prism elements in the input control file, are prism elements supported in HiFiLES?
Q…
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Using mission 3 for the standard 3-spline nozzle in driveNozzle.m gives an incorrect solution for the non-ideal nozzle, where flow remains subsonic throughout the nozzle instead of passing Mach 1 and …
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The simulation of inviscid supersonic air flowing over flat plate was tested. It ran on multi-CPUs(MPI)
It was always failed, and I could not find out any problems.
The flow parameters were as below:…
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FLOW:
- RX Frame
- Discard everything but Mode S DF11/17 and Mode A\C Emergency = true
frames.
- DF11, DF17:
- Check state:[ICAO as str] exists?
- No -> Create, set timeout, update state, set…
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could anyone help me?I have a question that I can not understand.in the cylinder testcase,The boundary conditions are "Sup_In "and"Sup_In ",why not "Sup_In "and"Sup_Out"?
And what is the differerence …
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```
This may be related to Issue 48, but I am having problems with
sprinklers. I have attached three input files. 'Simple Test_3.fds'
creates a compartment with gypsum board walls, no fire, and a …
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```
This may be related to Issue 48, but I am having problems with
sprinklers. I have attached three input files. 'Simple Test_3.fds'
creates a compartment with gypsum board walls, no fire, and a …
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Hi everybody,
i am using owncloud on virtual machine (Windows xp) since almost half a year (the shared folder is kind in a tunnel to my main system). Today i got the message "Csync konnte die journal …