Hi Junichi,

Thanks for trying out PyFR.

I set the initial velocity distribution using hyperbolic tangent function, and 
could run the case.

Great!

Current issues are shock wave generation from bottom of inlet as shown in the 
attached figure and termination of simulation job with an error message 
"RuntimeError: Minimum sized time step rejected". I'm trying to solve the issue.

May require some tuning of the artificial viscosity parameters - which can be a 
bit fiddly.

Cheers

Peter

Dr Peter Vincent MSci ARCS DIC PhD
Reader in Aeronautics and EPSRC Fellow
Department of Aeronautics
Imperial College London
South Kensington
London
SW7 2AZ
UK

web: 
www.imperial.ac.uk/aeronautics/research/vincentlab<http://www.imperial.ac.uk/aeronautics/research/vincentlab>
twitter: @Vincent_Lab<https://twitter.com/Vincent_Lab>





On 16 May 2017, at 15:55, Junichi Fukui 
<[email protected]<mailto:[email protected]>> wrote:

Hi Freddie,

Thank you for your advice.

I set the initial velocity distribution using hyperbolic tangent function, and 
could run the case.

Current issues are shock wave generation from bottom of inlet as shown in the 
attached figure and termination of simulation job with an error message 
"RuntimeError: Minimum sized time step rejected". I'm trying to solve the issue.

Thanks and regards,
Junichi

2017年5月15日月曜日 23時07分32秒 UTC+9 Freddie Witherden:
Hi Junichi,

On 15/05/2017 06:57, Junichi Fukui wrote:
> Dear all,
>
> I'm trying to solve supersonic cavity flow case at Mach 2.0 using PyFR
> 1.6.0. The attached files are mesh files and case setup file for the
> simulation. I would like to set zero velocity inside cavity region (Y <=
> 0), and uniform velocity (2.366431913, 0) with smooth velocity
> transition from non-slip wall in upper cavity region (Y > 0).
>
> How can we set the velocity distribution in [soln-ics] section of ini file?

The initial conditions can be a function of the spatial coordinates.  In
order to create a smooth step you can use a hyperbolic tangent.

Regards, Freddie.


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