Hi Zach,

I was interested in running a compressible simulation with PyFR.  The target 
Reynolds number would be 2.146e+06.

OK. Out of interest, what is the Mach number?

A p4 mesh would likely consist of around 15e+06 hexes.

OK. So this would have ~ 1.8Bn solution points.

Freddie’s spreadsheet, if I’m reading correctly, estimates a 3-D 
double-precision Navier-Stokes problem would require 3.7e+13 bytes or 35.2GiB 
of memory to run.

Do you mean 35 TB?

 Again, correct me if I’m wrong, but if I recall the tilmestep should be 
somewhere between 1/p and 1/p^2 which would be between 0.25 and 0.0625 for a 
4th order simulation.

The scaling with p is, as you suggest, somewhere between 1/p and 1/p^2. But the 
absolute value of the time-step will depend on how you have 
non-dimensionalised. It you have an inflow velocity of 1 and a characteristic 
length of 1 I would expect a tilmestep of ~ 1e-5 - 1e-6 at this Reynolds 
number, depending on mesh quality.

Ideally, I would like to run this out to steady state.

What do you mean by steady-state here, since the flow is turbulent? Do you mean 
run it long enough such that you can gather accurate statistics. Depending on 
the flow problem and the quantities you want to converge, this can mean running 
for 10-100s of characteristic flow passes.

AWS has p3 instances with 1, 4, and 8 NVIDIA V100 cards available each with 
16GB of memory, 5120 CUDA cores, and 7TFLOPS of double-precision performance.  
Is this problem tractable in the latest PyFR release?

We have never done a simulation at such a high Re. But it might be tractable.

 Does PyFR provide an inlet boundary condition where a total pressure and total 
temperature profile can be specified?

We have the sub-in-ftpttang BC, which I believe now can have a spatial 
dependence (someone can correct me if I am wrong).

Cheers

Peter

Dr Peter Vincent MSci ARCS DIC PhD FRAeS
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





On 8 Feb 2018, at 17:15, Zach Davis 
<zda...@pointwise.com<mailto:zda...@pointwise.com>> wrote:

All,

I was interested in running a compressible simulation with PyFR.  The target 
Reynolds number would be 2.146e+06.  A p4 mesh would likely consist of around 
15e+06 hexes.  Freddie’s spreadsheet, if I’m reading correctly, estimates a 3-D 
double-precision Navier-Stokes problem would require 3.7e+13 bytes or 35.2GiB 
of memory to run.  Again, correct me if I’m wrong, but if I recall the 
tilmestep should be somewhere between 1/p and 1/p^2 which would be between 0.25 
and 0.0625 for a 4th order simulation.  Ideally, I would like to run this out 
to steady state.

AWS has p3 instances with 1, 4, and 8 NVIDIA V100 cards available each with 
16GB of memory, 5120 CUDA cores, and 7TFLOPS of double-precision performance.  
Is this problem tractable in the latest PyFR release?  Does PyFR provide an 
inlet boundary condition where a total pressure and total temperature profile 
can be specified?

Best Regards,



[Pointwise, Inc.]
Zach Davis
Pointwise®, Inc.
Sr. Engineer, Sales & Marketing
213 South Jennings Avenue
Fort Worth, TX 76104-1107

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