|
|
List of indices to OUTPUT MATRIX - ignored? |
|
|
Save GMV data output (1 - last, 2 - every SAVEEVERYTIME, 3 - both ) |
|
|
Save TECPLOT data output |
|
|
Save TECPLOT(higher p) data output |
|
|
Save RESULTS output |
|
|
Save BINARY output |
|
|
Save PRESSURE/surface output |
|
|
INI file "femfluid.ini" |
|
|
LOG file "femfluid.log" |
|
|
"femfluid.dat" |
|
|
"report.txt" |
|
|
"results.txt" |
|
|
|
|
|
"triang" |
|
|
"triang.coarse" |
|
|
"solution" |
|
|
"reread.ini" |
|
|
"" |
|
|
"" |
|
|
"" |
|
|
"release" |
|
|
"pressure" |
|
|
"motion" |
|
|
"draglift" |
|
|
"freesurface" |
|
|
Number of Elements |
|
|
Number of Sides |
|
|
Number of Points/Vertices |
|
|
Number of Boundary Sides |
|
|
|
|
|
vertices location at current time level N |
|
|
boundary marks etc. |
|
|
|
|
|
|
|
|
vertices location at previous time level N-1 |
|
|
|
|
|
vertices location at previous time level N-2 |
|
|
|
|
|
|
|
|
initial/original configuration (ALE) |
|
|
whether to fix pressure at a point (when solving NS with just Dirichlet BC, -1 if no fix) |
|
|
Patch - indices to PatchList |
|
|
Patch - elements neighbouring each vertex |
|
|
Patch - for reconstruction near boundary |
|
|
|
|
|
previous grid velocity - piecewise linear |
|
|
|
|
|
|
|
|
current grid velocity |
|
|
|
|
|
|
|
|
Triangulation: list of elements vertices ELEMENT[index_element][index_of_vertex] |
|
|
Triangulation: element description |
|
|
Triangulation: indices of boundary sides |
|
|
list of sides vertices SIDE[index_side][index_of_vertex] |
|
|
length of side |
|
|
side description |
|
|
2 - boundary elements of a side (first with the same orientation??) |
|
|
List of boundary sides - sorted by Boundary Marks |
|
|
length of the maximal side |
|
|
length of the minimal side |
|
|
Number of Boundary Types |
|
|
Boundary Types Identification |
|
|
Number of Boundary with Prescribed BndrID |
|
|
Distance of the closest layer to the wall |
|
|
Dimension of the FEM space (one function = velocity component) |
|
|
Dimension of the FEM space for Pressure |
|
|
Global Indices of Element Base Functions |
|
|
Description of Base Functions |
|
|
Pressure Global Indices |
|
|
Description of Pressure Base Functions |
|
|
|
|
|
Indices of Bs Functions - side and nodal |
|
|
|
|
|
Description of Bs functions - side and noda |
|
|
|
|
|
(Pressure) Indices of Bs Functions - side and nodal |
|
|
|
|
|
(Pressure) Description of Bs functions - side and noda |
|
|
bndr side bs indices |
|
|
bndr side bs description |
|
|
pressure bndr side bs indices |
|
|
pressure bndr side description |
|
|
use geometrical nonlinearities |
|
|
10 - fixed domain, 20 - prescribed motion (2 degrees of freedom,given ampl. & freq. ) 30 - aeroelastic model (2 degrees of freedom) |
|
|
Fluid model (laminar/RANS+SA/RANS+SST) |
|
|
fixed/prescribed motion/ode/Lame |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
number of stationary iterations |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
mean value for rotation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
static components of aerod. forces |
|
|
|
|
|
elastic axis recent location |
|
|
|
|
|
elastic axis original location |
|
|
|
|
|
|
|
|
flap params |
|
|
|
|
|
|
|
|
flap params |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
polynomial degree for 1d and 2d |
|
|
|
|
|
number of q.nodes for 1d/2d |
|
|
|
|
|
1-dimensional quadrature formula knots and weights |
|
|
|
|
|
2-dimensional quadrature formula knots and weights |
|
|
|
|
|
(2nd formula) - polynomial degree for 1d and 2d |
|
|
|
|
|
(2nd formula) - number of q.nodes for 1d/2d |
|
|
|
|
|
(2nd formula) 1-dimensional quadrature formula knots and weights |
|
|
|
|
|
2-dimensional quadrature formula knots and weights |
|
|
Maximal Element Type for velocity-pressure couple of spaces (default Taylor-Hood):
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
base functions values on the reference triangle |
|
|
base functions values on the reference side |
|
|
base functions derivatives on the reference triangle |
|
|
base functions 2nd derivatives on the reference triangle |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
real fluid kinematic viscosity |
|
|
Reynolds number Re= L U /viscosity |
|
|
1/Reynolds - viscosity for dimensinless variables |
|
|
|
|
|
time step |
|
|
nondimensional time since the start |
|
|
reference length L |
|
|
reference velocity U |
|
|
reference depth D - 2D forces transformed to 3D |
|
|
density (fluid) |
|
|
fluid density |
|
|
gas density |
|
|
fluid visc. |
|
|
gas visc. |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
time in seconds |
|
|
inlet velocity - multiple of reference velocity |
|
|
pressure out |
|
|
pressure out at part 0 |
|
|
pressure out at part 1 |
|
|
pressure out at part 2 |
|
|
pressure out at part 3 |
|
|
pressure out at part 4 |
|
|
pressure out nondimensional |
|
|
pressure out at part 0 - nondimensional |
|
|
pressure out at part 1 - nondimensional |
|
|
pressure out at part 2 - nondimensional |
|
|
pressure out at part 3 - nondimensional |
|
|
pressure out at part 4 - nondimensional |
|
|
Maximum of Iterations - usually for Linear Solver |
|
|
time period and time step number of time iterations |
|
|
time period |
|
|
Maximum of Inner Iterations - GMRES iterations |
|
|
|
|
|
GMRES Restart |
|
|
Maximum of Nonlinear Iterations |
|
|
Maximum of FLUID-STRUCTURE interactions |
|
|
prescribed precision - absolute error - linear solver |
|
|
prescribed precision - linear solver |
|
|
prescribed precision - for inner iterations |
|
|
epsilon for time rezidual - for stationary solution |
|
|
nonlinear precision - absolute |
|
|
nonlinear precision - relative |
|
|
NEWTON precision |
|
|
ODE precision |
|
|
ITIME - time index |
|
|
save solution - per every time step |
|
|
linear solver - per every iteration |
|
|
inner preconditioner - per every iteration |
|
|
save pressure - per every time iteration |
|
|
theta for relaxation |
|
|
Load program variables from FILE - TRUE or FALSE |
|
|
|
|
|
|
|
|
|
|
|
Stabilization type: SUPG (10), GALS(50), SUBGRID(100), MODGALS(200) |
|
|
SUPG delta |
|
|
GRAD-DIV tau |
|
|
GALS - pressure |
|
|
ADC stabilization |
|
|
Choice of delta_K: default - 0 (equal order), 1000 - special for Taylor-Hood, 2000 - based on STANDARD |
|
|
Choice of local h: default - 1 , sqrt(Area) - 3, etc. |
|
|
Choice of norm(b): default 2 (mean), 1- maximal |
|
|
Global norm(b) |
|
|
Non-Newtonian rheology parametr (power) |
|
|
Non-Newtonian rheology parametr (regularization) |
|
|
Yield stress for Bingham fluid |
|
|
discretization triplet : ROW - index |
|
|
discretization triplet : COLUMN - index |
|
|
VALUE |
|
|
Number of Nonzeros in TRIPLET |
|
|
Maximum of allocated nonzeros |
|
|
Local function values for pcw linear |
|
|
Local function values for pcw linear |
|
|
Local function values for pcw linear |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Function values of piecewise linear functions |
|
|
Function values of piecewise linear functions |
|
|
Function values of piecewise linear functions |
|
|
Element values 1 |
|
|
Element values 2 |
|
|
Element values 3 |
|
|
Element values 4 |
|
|
Element values 5 |
|
|
Element values 6 |
|
|
Element values 7 |
|
|
Element values 8 |
|
|
Sparse matrix for ALE motion |
|
|
Preconditioner for ALE stiffness matrix |
|
|
|
|
|
|
|
|
whether to use ALE in conservative form |
|
|
how the grid velocity should be computed |
|
|
|
|
|
|
|
|
|
|
|
boundary condition storage - P1 projected only |
|
|
|
|
|
|
|
|
vectors for time steppings |
|
|
vectors - temporary |
|
|
vectors - temporary |
|
|
Turbulent viscosity for RANS(Reynolds Averaged Navier-Stokes) equations |
|
|
Distance from the nearest wall |
|
|
|
|
|
|
|
|
|
|
|
Spalart-Allmaras turbulent viscosity model |
|
|
|
|
|
|
|
|
k - turbulent kinetic energy |
|
|
|
|
|
|
|
|
omg - turbulent specific dissipation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
der. of velocity |
|
|
|
|
|
|
|
|
|
|
|
der. of variables A,B |
|
|
Aerodynamical Forces computation |
|
|
NONLINEAR SOLVER OUTPUT |
|
|
|
|
|
Number of nonlinear iteration, time needed for nonlinear iter |
|
|
Symbolic UMFPACK decomposition |
|
|
Numeric UMFPACK decomposition |
|
|
|
|
|
|
|
|
System of Linear Equations - Matrix |
|
|
Linear solver |
|
|
System of Linear Equations - Vector |
|
|
|
|
|
Jacobian of transformation FROM the reference triangle |
|
|
Inverse(M) - Jacobian of transformation TO the reference triangle |
|
|
|
|
|
|
|
|
|
|
|
element repr. of uvec2,uvec1,uvec0, convection and test function |
|
|
|
|
|
|
|
|
element repr. of basefuntions Bj and Bk |
|
|
|
|
|
|
|
|
element repr. of Spalart-Allmaras variables |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
element repr. of SST/k-omg model |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
point x=ii/20.0 is represented by pressure base functions IDXA[ii] and IDXB[ii] |
|
|
|
|
|
weights of IDXA and IDXB representation |
|
|
|
|
|
point x=ii/20.0 is represented by pressure base functions IDXA[ii] and IDXB[ii] |
|
|
|
|
|
weights of IDXA and IDXB representation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
10 - fixed domain, 20 - prescribed motion (2 degrees of freedom,given ampl. & freq. ) 30 - aeroelastic model (2 degrees of freedom) |
|
|
Fluid model (laminar/RANS+SA/RANS+SST) |
|
|
fixed/prescribed motion/ode/Lame |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
mean value for rotation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
static components of aerod. forces |
|
|
|
|
|
elastic axis recent location |
|
|
|
|
|
elastic axis original location |
|
|
|
|
|
|
|
|
flap params |
|
|
|
|
|
|
|
|
|
1.4.6