Difference between revisions of "Synthetic Turbulence Inflow Generator"
(→STGSpectra.dat) |
(→STGSpectra.dat) |
||
Line 106: | Line 106: | ||
32 alphaWave=0.01; | 32 alphaWave=0.01; | ||
33 setEps=17251.0; | 33 setEps=17251.0; | ||
+ | 34 | ||
+ | 35 | ||
+ | 36 %% Unfolding | ||
+ | 37 nprocs_Dir =strcat(num2str(nprocs),'-procs_case/'); | ||
+ | 38 [x,ien,surround_nodes] =importCords(x_Path,conn_PATH); | ||
+ | 39 d2wall =importD2Wall(d2wall_tech,x,d2wall_Path); | ||
+ | 40 | ||
+ | 41 | ||
+ | 42 %% Load in STGInflow and interpolate onto the inflow mesh | ||
+ | 43 STGInflow_Path=[Run_Dir,nprocs_Dir,'STGInflow.dat']; | ||
+ | 44 STGInflow=importSTGInflow(STGInflow_Path); | ||
+ | 45 | ||
+ | 46 [U,V,W,uu,vv,ww,uv,uw,vw,sclr1,sclr2,lt,eps,ch_decomp]=... | ||
+ | 47 interpSTG(STGInflow,x,d2wall);%x(:,2)); | ||
+ | 48 if(~isnan(setEps)) | ||
+ | 49 eps=ones(length(x),1).*setEps; | ||
+ | 50 end | ||
+ | |||
+ | |||
+ | This will be the standard format for many of the scripts in this subdirectory. | ||
+ | That is, | ||
+ | |||
+ | * Description/ Authors (ln 1->9) | ||
+ | * function call/ function call example (ln 12->13) | ||
+ | * Settings for each run (ln 15->33) | ||
+ | * Loadins from other files (ln 36->47) | ||
+ | * Execution of the script (ln 48->end) | ||
+ | |||
+ | === function call === | ||
+ | There are five inputs to this function call | ||
+ | * x_Path (str) | ||
+ | * conn_Path (str) | ||
+ | ** x_Path and conn_Path are strings that point to files that are able to be interpreted by importCords.m. ```When these files read-in a .crd .cnn type files, they will | ||
+ | * d2wall_Path (str) | ||
+ | * nprocs (int) | ||
=== STGRand.dat === | === STGRand.dat === |
Revision as of 12:39, 24 February 2021
Synthetic Turbulence Inflow Generator (STG)
Contents
Overview
The Synthetic Turbulence Inflow generator is a method to produce an inflow boundary condition that results in turbulent flow in a short downstream distance. This method is desired to be more computationally efficient than resolving a flow through from transition. This page will cover the workflow to produce the necessary auxiliary files as well as included specifications for the solver.inp file for running a simulation with the STG boundary condition. There are three auxiliary files that are needed for the method in the n-procs_case directory at runtime:
- STGInflow.dat
- STGSpectra.dat
- STGRand.dat
All of the mentioned MATLAB scripts in this page are in the STGInit subdirectory of the file structure contained in the PHASTA code-tree from github.
STGInflow.dat
This is a file that will contain the mean velocity profiles, mean cross correlation targets, and any additional turbulence modeled scalars.
STGSpectra.dat
This file will contain the N spectral modes for each node that has the STG the boundary condition.
STGRand.dat
This file will contain random numbers for the N spectral modes. This is not a spatially varying set of numbers as the spectra is.
Pre-Proccessing/Preparation of Auxiliary Files
Boundary Condition Attribute
Within the simmodeler or meshing tool, the face that is to have the STG boundary condition must have a specified SurfID attribute that will later match the specified in solver.inp. A typical value that has been given to this boundary condition within our group is 411.
STGInflow.dat
This auxiliary file will be required not only for the running of PHASTA, but also, will be required for the random number optimization. The user will need mean flow field data at the position of the inflow from some preliminary simulation such as RANS data or data repository. The code requires this file to have the following format:
N
d2wall_0 U_1(d2wall_0) U_2(d2wall_0) U_3(d2wall_0) uu(d2wall_0) vv(d2wall_0) ww(d2wall_0) uv(d2wall_0) uw(d2wall_0) vw(d2wall_0) sclr1(d2wall_0) sclr2(d2wall_0)
d2wall_1 U_1(d2wall_1) U_2(d2wall_1) U_3(d2wall_1) uu(d2wall_1) vv(d2wall_1) ww(d2wall_1) uv(d2wall_1) uw(d2wall_1) vw(d2wall_1) sclr1(d2wall_1) sclr2(d2wall_1)
d2wall_2 U_1(d2wall_2) U_2(d2wall_2) U_3(d2wall_2) uu(d2wall_2) vv(d2wall_2) ww(d2wall_2) uv(d2wall_2) uw(d2wall_2) vw(d2wall_2) sclr1(d2wall_2) sclr2(d2wall_2)
.
.
.
d2wall_N U_1(d2wall_N) U_2(d2wall_N) U_3(d2wall_N) uu(d2wall_N) vv(d2wall_N) ww(d2wall_N) uv(d2wall_N) uw(d2wall_N) vw(d2wall_N) sclr1(d2wall_N) sclr2(d2wall_N)
Where:
- N is the number of rows that this file contains. It is the number of nodes in the specially varying direction.
- d2wall is the distance to the wall
- U_i are the three components of the average velocity feild
- uu, vv, ww, uv, uw, vw are the averages of the Reynolds' stress tensor
- sclr1 and sclr2 are the scalars that represent the turbulence model.
The input profiles are varied by the type of auxiliary simulation. So the post-processing of that preliminary simulation will be varied and so the generation of this data is left to the user. However for creating the STGInflow.dat file it is useful to know the format that the fortran file reader is setup for. The below chunk of MATLAB code is useful once the profiles are known:
nPoints = length(d); [dSort,index]=sort(d); fid=fopen('STGINFLOWNAME.dat','w'); fprintf(fid,'%d\n',nPoints); for j=1:nPoints i=index(j); tmp=[d(i) u(i,:) R(i,:) nut(i)]; if (j~=nPoints) fprintf(fid,'%.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E\n',tmp); elseif (j==nPoints) fprintf(fid,'%.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E %.12E',tmp); end end fclose(fid);
STGSpectra.dat
This file will contain the spectral data at each nodal point within the mesh that is attributed with the STG attribute. To create this file we use the first of several scripts within the STGInit subdirectory of the github remote repository for PHASTA. Within MATLAB open STGspectra.m. The following is what you should see from the header of the file:
1 %% Create STGspectra.dat 2 % This script will produce spectral data for the implementation in PHASTA 3 % This script's intention is to move the spectral data calculation out of 4 % PHASTA so as to not require a call to PHASTA to gather such data. (A 5 % wasteful thing to do when large meshes are investigated) 6 7 % Authors: Ken Jansen, John Patterson 8 % Version: 1.0 9 % Last mod: 7/3/2020 10 11 12 %STGspectra('exampleInput/LES_DNS_ReL1M_2d_KEJ_SAVEFILE.mat','exampleInput/LES_DNS_ReL1M_2d_KEJ.cnnTet',1,'/projects/tools/Models/STG/STG_tests/Post/analizeRand/RunTetRand_newRAND_2/',8) 13 function []=STGspectra(x_Path,conn_PATH,d2wall_Path,Run_Dir,nprocs) 14 tic 15 %% Preliminary Settings 16 nu=1.5E-5; 17 18 %Specify how the d2wall field may be constructed 19 d2wall_tech='load';%'calculate ana'; 20 %Specify (if nessicary), the path of the nodal data of the d2wall field 21 d2wall_Path='d2wall_ana.mat';%'none'; 22 23 %Specify the method to determine the nodes of the STGInflow plane 24 STG_node_choose='min_x'; 25 26 %Spesify the method by which the mesh data is structured 27 struct_Spe='structured'; 28 29 %Settings found in solver.inp that are nessisary for using the 30 %STGInflow 31 deltaBL=0.05; 32 alphaWave=0.01; 33 setEps=17251.0; 34 35 36 %% Unfolding 37 nprocs_Dir =strcat(num2str(nprocs),'-procs_case/'); 38 [x,ien,surround_nodes] =importCords(x_Path,conn_PATH); 39 d2wall =importD2Wall(d2wall_tech,x,d2wall_Path); 40 41 42 %% Load in STGInflow and interpolate onto the inflow mesh 43 STGInflow_Path=[Run_Dir,nprocs_Dir,'STGInflow.dat']; 44 STGInflow=importSTGInflow(STGInflow_Path); 45 46 [U,V,W,uu,vv,ww,uv,uw,vw,sclr1,sclr2,lt,eps,ch_decomp]=... 47 interpSTG(STGInflow,x,d2wall);%x(:,2)); 48 if(~isnan(setEps)) 49 eps=ones(length(x),1).*setEps; 50 end
This will be the standard format for many of the scripts in this subdirectory.
That is,
- Description/ Authors (ln 1->9)
- function call/ function call example (ln 12->13)
- Settings for each run (ln 15->33)
- Loadins from other files (ln 36->47)
- Execution of the script (ln 48->end)
function call
There are five inputs to this function call
- x_Path (str)
- conn_Path (str)
- x_Path and conn_Path are strings that point to files that are able to be interpreted by importCords.m. ```When these files read-in a .crd .cnn type files, they will
- d2wall_Path (str)
- nprocs (int)