Develop (#90)

* add restart file

* Add files for unsteady CHT adjoint case. Mesh adn primal solution files.

* Regression test for dyn discadj fsi (#62)

* add regression test for dyn discadj fsi

* add element files

* switch to dat files

* remove gradient file

* Added little fluid mesh for heat transfer bc. This is the fluid zone of the multizone mesh. (#68)

* Created feature_turbo_bodyforce branch with testcase mesh

* Add mesh file and TargetEA.dat for PR 1329 (#65)

* Add mesh file and TargetEA.dat for PR 1329

* Add direct solution for adjoint calculation

* Replace with coarser mesh

* Update FFD box (#69)

* Update solution file (#72)

* added testcase for wallfunctions

* change filename

* update restart file

* moved flatplate testcase for wallfunctions into wallfunctions/flatplate

* Add periodic pins Testcase (#76)

* Test cases for turbulence modeling

Create a test cases directory to verify turbulence models and their variants. Done for the SA model. Selected the RANS/RAE2822 airfoil as test case.

* add flamelet testcase with lookup table

* Revert "add flamelet testcase with lookup table"

This reverts commit 9a584a1.

* rename viscwedge folder

* Updated reference gradient file in radiation/p1adjoint for the coupled RHT-CFD regression test. (#84)

Co-authored-by: Thomas Dick <[email protected]>

* update restart file after fix (#85)

* Feature species transport (#78)

* Add passive species transport mesh and gmsh geo.

* Add primitive venturi mesh for species mixing.

* convert cgns test to hdf5

* Feature sobolev smoothing solver (#88)


* Sobolev gradient smoothing test case meshes and solution files added.

* Updated reference file for the Coupled RHT-CFD Adjoint test case in serial_regression_AD.py.

* Adapted reference files for Sobolev smoothing regression test after latest commits.

* Fixed an inconsistency in grad_smooth/naca0012/of_hess.dat.ref

* Adapted grad_smooth tests for new accuracy setting.

* Adopted grad_smooth regression tests for change to SU2_DOT_AD.

* moved filediff reference files to main SU2 repo and made NACA0012 mesh a symlink.

Co-authored-by: Thomas Dick <[email protected]>

Co-authored-by: TobiKattmann <[email protected]>
Co-authored-by: Charanya <[email protected]>
Co-authored-by: Wally Maier <[email protected]>
Co-authored-by: TobiKattmann <[email protected]>
Co-authored-by: EvertBunschoten <[email protected]>
Co-authored-by: snow54 <[email protected]>
Co-authored-by: bigfooted <[email protected]>
Co-authored-by: FlorianDm <[email protected]>
Co-authored-by: Florian <[email protected]>
Co-authored-by: Nijso <[email protected]>
Co-authored-by: Guillermo Suarez <[email protected]>
Co-authored-by: nbe0dev <[email protected]>
Co-authored-by: suargi <[email protected]>
Co-authored-by: thomasdick <[email protected]>
Co-authored-by: Thomas Dick <[email protected]>
Co-authored-by: Mickael Philit <[email protected]>

Author: 12 people

axisymmetric_rans/air_nozzle/solution_flow.dat

@@ -0,0 +1 @@
+../../euler/naca0012/mesh_NACA0012_inv.su2

euler/wedge/mesh_wedge_inv.cgns

@@ -1,6 +1,6 @@
 "VARIABLE"      , "GRADIENT"      , "FINDIFF_STEP"  
 0               , -0.000954218    , 0.001           
-1               , -0.00432385     , 0.001           
+1               , -0.00432384     , 0.001           
 2               , -0.0111485      , 0.001           
 3               , -0.0214656      , 0.001           
 4               , -0.0344212      , 0.001           

grad_smooth/naca0012/mesh_NACA0012_inv.su2

@@ -0,0 +1,92 @@
+// ----------------------------------------------------------------------------------- //
+// Tobias Kattmann, 24.09.2021, 2D rectangle for mixing validation testcase
+// ----------------------------------------------------------------------------------- //
+
+// Evoque Meshing Algorithm?
+Do_Meshing= 1; // 0=false, 1=true
+// Write Mesh files in .su2 format
+Write_mesh= 1; // 0=false, 1=true
+
+// Geometric inputs
+length= 10; // downstream direction
+height= 5; // crossstream direction, full length
+border= 1; // height of gas inlet, height-border= air inlet length
+
+// Mesh sizing inputs. Note that the #cells+Prgression needs some fiddeling such that mesh size at the border fits.
+Nl= 50; // Nodes in 'l'ength direction
+Nhg= 25; // Nodes in 'h eight direction of the 'g'as side
+Rhg= 0.9; // Progression of gas side [0,1], lower means more agressive
+Nha= 40; // Nodes in 'h eight direction of the 'a'ir side
+Rha= 0.9; // Progression of air side [0,1], lower means more agressive
+
+gridsize= 0.1; // Later on not important as structured mesh is achieved
+
+// ----------------------------------------------------------------------------------- //
+// POINTS
+
+// Starting in the origin, which is the most low-left point, and going clockwise.
+
+Point(1) = {0, 0, 0, gridsize};
+Point(2) = {0, border, 0, gridsize};
+Point(3) = {0, height, 0, gridsize};
+Point(4) = {length, height, 0, gridsize};
+Point(5) = {length, border, 0, gridsize};
+Point(6) = {length, 0, 0, gridsize};
+
+// ----------------------------------------------------------------------------------- //
+// LINES
+
+// gas inlet 
+Line(1) = {1,2};
+// air inlet
+Line(2) = {2,3};
+// top sym
+Line(3) = {3,4};
+// air outlet
+Line(4) = {4,5};
+// gas outlet
+Line(5) = {5,6};
+// bottom sym
+Line(6) = {6,1};
+// species border
+Line(7) = {2,5};
+
+// ----------------------------------------------------------------------------------- //
+// SURFACES (and Lineloops)
+Curve Loop(1) = {6, 1, 7, 5};  Plane Surface(1) = {1}; // gas box
+Curve Loop(2) = {3, 4, -7, 2}; Plane Surface(2) = {2}; // air box
+
+// make structured mesh with transfinite Lines
+// NOTE: The usage of Nwall and the progression has to be tuned again for any changes.
+Transfinite Line{3,-6,7} = Nl ; // downstream direction, no progression
+Transfinite Line{1,-5} = Nhg Using Progression Rhg; // gas side, progression towards border
+Transfinite Line{-2,4} = Nha Using Progression Rha; // air side, progression towards border
+
+// ----------------------------------------------------------------------------------- //
+// PHYSICAL GROUPS
+
+Physical Line("gas_inlet") = {1};
+Physical Line("air_inlet") = {2};
+Physical Line("outlet") = {4,5};
+Physical Line("top") = {3};
+Physical Line("bottom") = {6};
+
+Physical Surface("fluid") = {1,2};
+
+// ----------------------------------------------------------------------------------- //
+// Meshing
+Transfinite Surface "*";
+Recombine Surface "*";
+
+If (Do_Meshing == 1)
+    Mesh 1; Mesh 2;
+EndIf
+
+// ----------------------------------------------------------------------------------- //
+// Write .su2 meshfile
+If (Write_mesh == 1)
+
+    Mesh.Format = 42; // .su2 mesh format, 
+    Save "rectangle_mixing.su2";
+
+EndIf