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ENH: improve/verify atmBoundaryLayerInlet conditions
ENH: add generalised log-law type ground-normal inflow boundary conditions for wind velocity and turbulence quantities for homogeneous, two-dimensional, dry-air, equilibrium and neutral atmospheric boundary layer (ABL) modelling ENH: remove `zGround` entry, which is now automatically computed ENH: add `displacement height` entry, `d` ENH: add generalised atmBoundaryLayerInletOmega boundary condition ENH: add a verification case for atmBoundaryLayerInlet BCs DOC: improve atmBoundaryLayerInlet header documentation BUG: fix value-entry behaviour in atmBoundaryLayerInlet (fixes #1578) Without this change: - for serial-parallel computations, if `value` entry is available in an `atmBoundaryLayerInlet` BC, the theoretical ABL profile expressions are not computed, and the `value` entry content is used as a profile data - for parallel computations, if `value` entry is not available, `decomposePar` could not be executed. With this change: - assuming `value` entry is always be present, the use of `value` entry for the ABL profile specification is determined by a flag `initABL` - the default value of the optional flag `initABL` is `true`, but whenever `initABL=true` is executed, `initABL` is overwritten as `false` for the subsequent runs, so that `value` entry can be safely used. Thanks Per Jørgensen for the bug report. BUG: ensure atmBoundaryInlet conditions are Galilean-invariant (fixes #1692) Related references: The ground-normal profile expressions (tag:RH): Richards, P. J., & Hoxey, R. P. (1993). Appropriate boundary conditions for computational wind engineering models using the k-ε turbulence model. In Computational Wind Engineering 1 (pp. 145-153). DOI:10.1016/B978-0-444-81688-7.50018-8 Modifications to preserve the profiles downstream (tag:HW): Hargreaves, D. M., & Wright, N. G. (2007). On the use of the k–ε model in commercial CFD software to model the neutral atmospheric boundary layer. Journal of wind engineering and industrial aerodynamics, 95(5), 355-369. DOI:10.1016/j.jweia.2006.08.002 Expression generalisations to allow height variation for turbulence quantities (tag:YGCJ): Yang, Y., Gu, M., Chen, S., & Jin, X. (2009). New inflow boundary conditions for modelling the neutral equilibrium atmospheric boundary layer in computational wind engineering. J. of Wind Engineering and Industrial Aerodynamics, 97(2), 88-95. DOI:10.1016/j.jweia.2008.12.001 The generalised ground-normal profile expression for omega (tag:YGJ): Yang, Y., Gu, M., & Jin, X., (2009). New inflow boundary conditions for modelling the neutral equilibrium atmospheric boundary layer in SST k-ω model. In: The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, Taipei, Taiwan. Reproduced benchmark: Rectangular prism shown in FIG 1 of Hargreaves, D. M., & Wright, N. G. (2007). On the use of the k–ε model in commercial CFD software to model the neutral atmospheric boundary layer. Journal of wind engineering and industrial aerodynamics, 95(5), 355-369. DOI:10.1016/j.jweia.2006.08.002 Benchmark data: HW, 2007 FIG 6 TUT: update simpleFoam/turbineSiting tutorial accordingly
This commit is contained in:
Kutalmis Bercin
committed by
Andrew Heather
Andrew Heather
parent
5863c94be0
commit
336fb3bddf
@ -0,0 +1,66 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volVectorField;
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object U;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 1 -1 0 0 0 0];
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internalField uniform (0 0 0);
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boundaryField
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{
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inlet
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{
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type atmBoundaryLayerInletVelocity;
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#include "include/ABLConditions"
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value uniform (0 0 0);
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}
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ground
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{
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type noSlip;
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}
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top
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{
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// (HW:p. 365):
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// "In addition, as suggested by RH and often ignored by others, a"
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// "constant shear stress of rho*(u^*)^2 was applied at the top boundary."
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//
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// u^* ~ Uref*kappa/ln((Zref+z0)/z0)
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// (HW:Table 1):
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// Uref = 10 m/s
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// Zref = 6 m
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// z0 = 0.01 m
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// tau = rho*(u^*)^2 = 0.390796574
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type fixedShearStress;
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tau (0.390796574 0 0);
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value uniform (0 0 0);
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type inletOutlet;
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inletValue uniform (0 0 0);
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value $internalField;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,59 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object epsilon;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -3 0 0 0 0];
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internalField uniform 0.01;
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boundaryField
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{
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#include "include/ABLConditions"
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inlet
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{
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type atmBoundaryLayerInletEpsilon;
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#include "include/ABLConditions"
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value uniform 0;
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}
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ground
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{
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type epsilonWallFunction;
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Cmu $Cmu;
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kappa $kappa;
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value $internalField;
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}
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top
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{
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type zeroGradient;
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,19 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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kappa 0.40; // (HW:p. 358)
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Cmu 0.09; // (HW:p. 358)
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flowDir (1 0 0); // (HW:Fig. 1)
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zDir (0 0 1); // (HW:Fig. 1)
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Uref 10.0; // (HW:Table 1)
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Zref 6.0; // (HW:Table 1)
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z0 uniform 0.01; // (HW:Table 1)
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d uniform 0.0;
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// ************************************************************************* //
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@ -0,0 +1,55 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object k;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -2 0 0 0 0];
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internalField uniform 1.3; // (HW:Eq. 6)
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boundaryField
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{
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inlet
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{
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type atmBoundaryLayerInletK;
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#include "include/ABLConditions"
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value uniform 0;
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}
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ground
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{
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type kqRWallFunction;
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value uniform 0.0;
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}
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top
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{
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type zeroGradient;
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,59 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object nut;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -1 0 0 0 0];
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internalField uniform 0;
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boundaryField
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{
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#include "include/ABLConditions"
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inlet
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{
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type calculated;
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value uniform 0;
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}
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ground
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{
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type nutkAtmRoughWallFunction;
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kappa $kappa;
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Cmu $Cmu;
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z0 $z0;
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value uniform 0.0;
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}
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top
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{
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type calculated;
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value uniform 0;
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type calculated;
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value uniform 0;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,59 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object omega;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 0 -1 0 0 0 0];
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internalField uniform 0.0007;
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boundaryField
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{
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#include "include/ABLConditions"
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inlet
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{
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type atmBoundaryLayerInletOmega;
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#include "include/ABLConditions"
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value uniform 0;
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}
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ground
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{
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type omegaWallFunction;
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Cmu $Cmu;
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kappa $kappa;
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value $internalField;
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}
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top
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{
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type zeroGradient;
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,51 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v1912 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object p;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -2 0 0 0 0];
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internalField uniform 0;
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boundaryField
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{
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inlet
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{
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type zeroGradient;
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}
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ground
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{
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type zeroGradient;
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}
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top
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{
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type zeroGradient;
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}
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sides
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{
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type symmetry;
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}
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outlet
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{
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type uniformFixedValue;
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uniformValue constant 0;
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,12 @@
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#!/bin/sh
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cd "${0%/*}" || exit # Run from this directory
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. ${WM_PROJECT_DIR:?}/bin/tools/CleanFunctions # Tutorial clean functions
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#------------------------------------------------------------------------------
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cleanCase0
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rm -rf plots
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rm -f constant/turbulenceProperties
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rm -rf system/atm-HargreavesWright-2007
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#------------------------------------------------------------------------------
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@ -0,0 +1,21 @@
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#!/bin/sh
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cd "${0%/*}" || exit # Run from this directory
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. ${WM_PROJECT_DIR:?}/bin/tools/RunFunctions # Tutorial run functions
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#------------------------------------------------------------------------------
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restore0Dir
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cp -rf $FOAM_TUTORIALS/resources/dataset/atm-HargreavesWright-2007 system/.
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rasModel="kEpsilon" # Tested options="kOmegaSST","kEpsilon"
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sed "s|RAS_MODEL|$rasModel|g" constant/turbulenceProperties.template > \
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constant/turbulenceProperties
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runApplication blockMesh
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runApplication renumberMesh -overwrite
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runApplication $(getApplication)
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#------------------------------------------------------------------------------
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@ -0,0 +1,21 @@
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#!/bin/sh
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cd "${0%/*}" || exit # Run from this directory
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. ${WM_PROJECT_DIR:?}/bin/tools/RunFunctions # Tutorial run functions
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#------------------------------------------------------------------------------
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restore0Dir
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rasModel="kEpsilon" # Tested options="kOmegaSST","kEpsilon"
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sed "s|RAS_MODEL|$rasModel|g" constant/turbulenceProperties.template > \
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constant/turbulenceProperties
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runApplication blockMesh
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runApplication decomposePar
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runParallel renumberMesh -overwrite
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runParallel $(getApplication)
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#------------------------------------------------------------------------------
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@ -0,0 +1,117 @@
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#------------------------------------------------------------------------------
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Overview
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"By setting appropriate profiles for wind velocity and the turbulence
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quantities at the inlet, it is often assumed that the boundary layer will
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be maintained up to the buildings or obstructions in the flow." (HW:p. 355).
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However, it was quantified by (HW:p. 355) that "even in the absence of
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obstructions, ..., the velocity and turbulence profiles decay along the
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fetch" (HW:p. 355). It was shown by (HW:p. 355) that a set of modifications
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were required to maintain a neutral atmospheric boundary layer throughout
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an empty and long computational domain of a RANS computation.
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Aim:
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Verification of the following boundary conditions in terms of the
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maintenance of inlet quantities downstream within a RANS computation:
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- atmBoundaryLayerInletVelocity
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- atmBoundaryLayerInletK
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- atmBoundaryLayerInletEpsilon
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- atmBoundaryLayerInletOmega
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Benchmark (Physical phenomenon):
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The benchmark is an empty fetch computational domain, steady-state
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RANS simulation involving the following traits:
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- External flow
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- The surface layer portion of the neutral-stratified equilibrium
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atmospheric boundary layer (no Ekman layer)
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- Dry air
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- Homogeneous, smooth terrain
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- Spatiotemporal-invariant aerodynamic roughness length
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- No displacement height
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- Newtonian, single-phase, incompressible, non-reacting
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Benchmark scenario:
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- Computational domain: (HW:Fig. 1)
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- Benchmark dataset: (HW:Fig. 6) (Obtained by the WebPlotDigitizer-4.2
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(Rohatgi, 2019))
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Resources:
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Computational study (tag:HW):
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Hargreaves, D. M., & Wright, N. G. (2007).
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On the use of the k–ε model in commercial CFD software
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to model the neutral atmospheric boundary layer.
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Journal of wind engineering and
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industrial aerodynamics, 95(5), 355-369.
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DOI:10.1016/j.jweia.2006.08.002
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Wind profile (tag:RQP):
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Richards, P. J., Quinn, A. D., & Parker, S. (2002).
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A 6 m cube in an atmospheric boundary layer flow-Part 2.
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Computational solutions. Wind and structures, 5(2_3_4), 177-192.
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DOI:10.12989/was.2002.5.2_3_4.177
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Physical modelling:
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- The governing equations for:
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- Steady-state, Newtonian, single-phase, incompressible fluid flows,
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excluding any thermal chemical, electromagnetic and scalar
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interactions
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- Mathematical approach for the turbulence modelling:
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- Reynolds-averaged Navier-Stokes simulation (RANS)
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- Turbulence closure model:
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- kEpsilon and kOmegaSST linear eddy viscosity closure models
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- The sets of input (HW:Table 1):
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- Reference height, Zref = 6 [m]
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- Aerodynamic roughness height, z0 = 0.01 [m]
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- Displacement height, d = 0 [m]
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- Reference mean wind speed, Uref = 10 [m/s]
|
||||
|
||||
Computational domain modelling:
|
||||
|
||||
- Rectangular prism
|
||||
- (x1, x2, x3)
|
||||
= (5000, 100, 500) [m]
|
||||
= (streamwise, spanwise, ground-normal) directions
|
||||
|
||||
Computational domain discretisation:
|
||||
|
||||
- Spatial resolution:
|
||||
- (x1, x2, x3) = (500, 5, 50) [cells]
|
||||
- Refer to the `system/blockMeshDict` for the grading details
|
||||
- Temporal resolution: Steady state
|
||||
|
||||
Equation discretisation:
|
||||
|
||||
- Spatial derivatives and variables:
|
||||
- Convection: Second order
|
||||
- Others: Second order with various limiters
|
||||
|
||||
- Temporal derivatives and variables: First order
|
||||
|
||||
Numerical boundary/initial conditions:
|
||||
|
||||
- Refer to `0.orig`
|
||||
|
||||
Pressure-velocity coupling algorithm:
|
||||
|
||||
- SIMPLEC
|
||||
|
||||
Linear solvers:
|
||||
|
||||
- Refer to `system/fvSolution`
|
||||
|
||||
Initialisation and sampling:
|
||||
|
||||
- No initialisation/averaging
|
||||
- Sampling at the end of the simulation via `system/sampleDict`
|
||||
- Refer to `system/controlDict` for further details
|
||||
|
||||
|
||||
#------------------------------------------------------------------------------
|
||||
@ -0,0 +1,22 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object transportProperties;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
transportModel Newtonian;
|
||||
|
||||
nu 1.5e-05;
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,42 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object turbulenceProperties;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
simulationType RAS;
|
||||
|
||||
RAS
|
||||
{
|
||||
RASModel RAS_MODEL;
|
||||
turbulence on;
|
||||
printCoeffs on;
|
||||
|
||||
RAS_MODELCoeffs // Valid only for epsilon-based models
|
||||
{
|
||||
Cmu 0.09;
|
||||
C1 1.44;
|
||||
C2 1.92;
|
||||
sigmaEps 1.11; //Original value:1.44
|
||||
// See p. 358:
|
||||
// Hargreaves, D. M., & Wright, N. G. (2007).
|
||||
// On the use of the k–ε model in commercial CFD software
|
||||
// to model the neutral atmospheric boundary layer.
|
||||
// Journal of wind engineering and
|
||||
// industrial aerodynamics, 95(5), 355-369.
|
||||
// DOI:10.1016/j.jweia.2006.08.002
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
339
tutorials/verificationAndValidation/atmosphericModels/HargreavesWright_2007/plot
Executable file
339
tutorials/verificationAndValidation/atmosphericModels/HargreavesWright_2007/plot
Executable file
@ -0,0 +1,339 @@
|
||||
#!/bin/sh
|
||||
cd "${0%/*}" || exit # Run from this directory
|
||||
. ${WM_PROJECT_DIR:?}/bin/tools/RunFunctions # Tutorial run functions
|
||||
#------------------------------------------------------------------------------
|
||||
|
||||
# Postprocess according to the existence of "epsilon" or "omega"
|
||||
baseEpsilonOrOmega="epsilon" # options: "epsilon", "omega".
|
||||
|
||||
# Note: Benchmark data is available for the standard k-epsilon model from:
|
||||
# Hargreaves, D. M., & Wright, N. G. (2007).
|
||||
# On the use of the k–ε model in commercial CFD software
|
||||
# to model the neutral atmospheric boundary layer.
|
||||
# Journal of wind engineering and
|
||||
# industrial aerodynamics, 95(5), 355-369.
|
||||
# DOI:10.1016/j.jweia.2006.08.002
|
||||
# Figure 6.
|
||||
#------------------------------------------------------------------------------
|
||||
|
||||
plotUxUpstream() {
|
||||
timeDir=$1
|
||||
zMin=$2
|
||||
echo " Plotting the ground-normal flow speed profile (upstream)."
|
||||
|
||||
outName="plots/Ux_upstream.png"
|
||||
gnuplot<<PLT_UX_UPSTREAM
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [4:18]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top left
|
||||
set xlabel "Ux [m s^{-1}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp0="$timeDir/x_0mCell_U.xy"
|
||||
inp1="$timeDir/x_0mPatch_U.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp0 u 2:((\$1-$zMin)/zRef) t "OF, x=0m (Patch)" w l lw 2 lc rgb "#009E73", \
|
||||
inp1 u 2:((\$1-$zMin)/zRef) t "OF, x=0m (Cell)" w l lw 2 lc rgb "#F0E440"
|
||||
PLT_UX_UPSTREAM
|
||||
}
|
||||
|
||||
|
||||
plotUxMid() {
|
||||
timeDir=$1
|
||||
zMin=$2
|
||||
echo " Plotting the ground-normal flow speed profile (mid-range)."
|
||||
|
||||
outName="plots/Ux_mid.png"
|
||||
gnuplot<<PLT_UX_MID
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [4:18]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top left
|
||||
set xlabel "Ux [m s^{-1}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp2="$timeDir/x_2500m_U.xy"
|
||||
inp3="$timeDir/x_4000m_U.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp2 u 2:((\$1-$zMin)/zRef) t "OF, x=2500m" w l lw 2 lc rgb "#0072B2", \
|
||||
inp3 u 2:((\$1-$zMin)/zRef) t "OF, x=4000m" w l lw 2 lc rgb "#D55E00"
|
||||
PLT_UX_MID
|
||||
}
|
||||
|
||||
|
||||
plotUxDownstream() {
|
||||
timeDir=$1
|
||||
zMin=$2
|
||||
echo " Plotting the ground-normal flow speed profile (downstream)."
|
||||
|
||||
outName="plots/Ux_downstream.png"
|
||||
gnuplot<<PLT_UX_DOWNSTREAM
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [4:18]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top left
|
||||
set xlabel "Ux [m s^{-1}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp4="$timeDir/x_5000mCell_U.xy"
|
||||
inp5="$timeDir/x_5000mPatch_U.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/Ux-HW-RH-Fig6a" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp4 u 2:((\$1-$zMin)/zRef) t "OF, x=5000m (Cell)" w l lw 2 lc rgb "#CC79A7", \
|
||||
inp5 u 2:((\$1-$zMin)/zRef) t "OF, x=5000m (Patch)" w l lw 2 lc rgb "#440154"
|
||||
PLT_UX_DOWNSTREAM
|
||||
}
|
||||
|
||||
|
||||
plotK() {
|
||||
timeDir=$1
|
||||
items=$2
|
||||
seq=$3
|
||||
zMin=$4
|
||||
echo " Plotting the ground-normal turbulent kinetic energy profile."
|
||||
|
||||
outName="plots/k.png"
|
||||
gnuplot<<PLT_K
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [1:2]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top right
|
||||
set xlabel "k [m^2 s^{-2}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp0="$timeDir/x_0mCell_$items.xy"
|
||||
inp1="$timeDir/x_0mPatch_$items.xy"
|
||||
inp2="$timeDir/x_2500m_$items.xy"
|
||||
inp3="$timeDir/x_4000m_$items.xy"
|
||||
inp4="$timeDir/x_5000mCell_$items.xy"
|
||||
inp5="$timeDir/x_5000mPatch_$items.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/k-RH-Fig6b" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/k-HW-Fig6b-2500" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/k-HW-Fig6b-4000" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp0 u $seq:((\$1-$zMin)/zRef) t "OF, x=0m (Patch)" w l lw 2 lc rgb "#009E73", \
|
||||
inp1 u $seq:((\$1-$zMin)/zRef) t "OF, x=0m (Cell)" w l lw 2 lc rgb "#F0E440", \
|
||||
inp2 u $seq:((\$1-$zMin)/zRef) t "OF, x=2500m" w l lw 2 lc rgb "#0072B2", \
|
||||
inp3 u $seq:((\$1-$zMin)/zRef) t "OF, x=4000m" w l lw 2 lc rgb "#D55E00", \
|
||||
inp4 u $seq:((\$1-$zMin)/zRef) t "OF, x=5000m (Cell)" w l lw 2 lc rgb "#CC79A7", \
|
||||
inp5 u $seq:((\$1-$zMin)/zRef) t "OF, x=5000m (Patch)" w l lw 2 lc rgb "#440154"
|
||||
PLT_K
|
||||
}
|
||||
|
||||
|
||||
plotEpsilon() {
|
||||
timeDir=$1
|
||||
items=$2
|
||||
zMin=$3
|
||||
echo " Plotting the ground-normal turbulent kinetic"\
|
||||
"energy dissipation rate profile."
|
||||
|
||||
outName="plots/epsilon.png"
|
||||
gnuplot<<PLT_EPSILON
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [0.001:10]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top right
|
||||
set xlabel "epsilon [m^2 s^{-3}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set logscale x
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp0="$timeDir/x_0mCell_$items.xy"
|
||||
inp1="$timeDir/x_0mPatch_$items.xy"
|
||||
inp2="$timeDir/x_2500m_$items.xy"
|
||||
inp3="$timeDir/x_4000m_$items.xy"
|
||||
inp4="$timeDir/x_5000mCell_$items.xy"
|
||||
inp5="$timeDir/x_5000mPatch_$items.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/epsilon-HW-RH-Fig6c" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/epsilon-HW-RH-Fig6c" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/epsilon-HW-RH-Fig6c" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp0 u 2:((\$1-$zMin)/zRef) t "OF, x=0m (Patch)" w l lw 2 lc rgb "#009E73", \
|
||||
inp1 u 2:((\$1-$zMin)/zRef) t "OF, x=0m (Cell)" w l lw 2 lc rgb "#F0E440", \
|
||||
inp2 u 2:((\$1-$zMin)/zRef) t "OF, x=2500m" w l lw 2 lc rgb "#0072B2", \
|
||||
inp3 u 2:((\$1-$zMin)/zRef) t "OF, x=4000m" w l lw 2 lc rgb "#D55E00", \
|
||||
inp4 u 2:((\$1-$zMin)/zRef) t "OF, x=5000m (Cell)" w l lw 2 lc rgb "#CC79A7", \
|
||||
inp5 u 2:((\$1-$zMin)/zRef) t "OF, x=5000m (Patch)" w l lw 2 lc rgb "#440154"
|
||||
PLT_EPSILON
|
||||
}
|
||||
|
||||
|
||||
plotOmega() {
|
||||
timeDir=$1
|
||||
items=$2
|
||||
zMin=$3
|
||||
echo " Plotting the ground-normal specific dissipation rate profile."
|
||||
|
||||
outName="plots/omega.png"
|
||||
gnuplot<<PLT_OMEGA
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [0.001:10]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key top right
|
||||
set xlabel "omega [s^{-1}]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set logscale x
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp0="$timeDir/x_0mCell_$items.xy"
|
||||
inp1="$timeDir/x_0mPatch_$items.xy"
|
||||
inp2="$timeDir/x_2500m_$items.xy"
|
||||
inp3="$timeDir/x_4000m_$items.xy"
|
||||
inp4="$timeDir/x_5000mCell_$items.xy"
|
||||
inp5="$timeDir/x_5000mPatch_$items.xy"
|
||||
|
||||
plot \
|
||||
inp0 u 4:((\$1-$zMin)/zRef) t "OF, x=0m (Patch)" w l lw 2 lc rgb "#009E73", \
|
||||
inp1 u 4:((\$1-$zMin)/zRef) t "OF, x=0m (Cell)" w l lw 2 lc rgb "#F0E440", \
|
||||
inp2 u 4:((\$1-$zMin)/zRef) t "OF, x=2500m" w l lw 2 lc rgb "#0072B2", \
|
||||
inp3 u 4:((\$1-$zMin)/zRef) t "OF, x=4000m" w l lw 2 lc rgb "#D55E00", \
|
||||
inp4 u 4:((\$1-$zMin)/zRef) t "OF, x=5000m (Cell)" w l lw 2 lc rgb "#CC79A7", \
|
||||
inp5 u 4:((\$1-$zMin)/zRef) t "OF, x=5000m (Patch)" w l lw 2 lc rgb "#440154"
|
||||
PLT_OMEGA
|
||||
}
|
||||
|
||||
|
||||
plotMut() {
|
||||
timeDir=$1
|
||||
items=$2
|
||||
seq=$3
|
||||
zMin=$4
|
||||
echo " Plotting the ground-normal turbulent viscosity profile."
|
||||
|
||||
outName="plots/mut.png"
|
||||
gnuplot<<PLT_MUT
|
||||
set terminal pngcairo font "helvetica,20" size 1000, 800
|
||||
set xrange [0:120]
|
||||
set yrange [0:50]
|
||||
set grid
|
||||
set key bottom right
|
||||
set xlabel "mu_t [Pa.s]"
|
||||
set ylabel "Non-dimensionalised height, z/z_{ref}"
|
||||
set offset .05, .05
|
||||
set output "$outName"
|
||||
|
||||
zRef = 6
|
||||
inp0="$timeDir/x_0mCell_$items.xy"
|
||||
inp1="$timeDir/x_0mPatch_$items.xy"
|
||||
inp2="$timeDir/x_2500m_$items.xy"
|
||||
inp3="$timeDir/x_4000m_$items.xy"
|
||||
inp4="$timeDir/x_5000mCell_$items.xy"
|
||||
inp5="$timeDir/x_5000mPatch_$items.xy"
|
||||
|
||||
plot \
|
||||
"system/benchmark-data-HargreavesWright2007/mut-RH-Fig6d" \
|
||||
u 1:2 t "RH" w p ps 2 pt 6 lc rgb "#000000", \
|
||||
"system/benchmark-data-HargreavesWright2007/mut-HW-Fig6d-2500" \
|
||||
u 1:2 t "HW, x=2500m" w p ps 1 pt 5 lc rgb "#E69F00", \
|
||||
"system/benchmark-data-HargreavesWright2007/mut-HW-Fig6d-4000" \
|
||||
u 1:2 t "HW, x=4000m" w p ps 0.5 pt 4 lc rgb "#56B4E9", \
|
||||
inp0 u $seq:((\$1-$zMin)/zRef) t "OF, x=0m (Patch)" w l lw 2 lc rgb "#009E73", \
|
||||
inp1 u $seq:((\$1-$zMin)/zRef) t "OF, x=0m (Cell)" w l lw 2 lc rgb "#F0E440", \
|
||||
inp2 u $seq:((\$1-$zMin)/zRef) t "OF, x=2500m" w l lw 2 lc rgb "#0072B2", \
|
||||
inp3 u $seq:((\$1-$zMin)/zRef) t "OF, x=4000m" w l lw 2 lc rgb "#D55E00", \
|
||||
inp4 u $seq:((\$1-$zMin)/zRef) t "OF, x=5000m (Cell)" w l lw 2 lc rgb "#CC79A7", \
|
||||
inp5 u $seq:((\$1-$zMin)/zRef) t "OF, x=5000m (Patch)" w l lw 2 lc rgb "#440154"
|
||||
PLT_MUT
|
||||
}
|
||||
|
||||
|
||||
#------------------------------------------------------------------------------
|
||||
|
||||
# Require gnuplot
|
||||
command -v gnuplot >/dev/null || {
|
||||
echo "gnuplot not found - skipping graph creation" 1>&2
|
||||
exit 1
|
||||
}
|
||||
|
||||
# The latestTime in postProcessing/samples
|
||||
timeDir=$(foamListTimes -case postProcessing/samples -latestTime 2>/dev/null)
|
||||
[ -n "$timeDir" ] || {
|
||||
echo "No postProcessing/samples found - skipping graph creation" 1>&2
|
||||
exit 2
|
||||
}
|
||||
timeDir="postProcessing/samples/$timeDir"
|
||||
zMin=0
|
||||
mkdir -p plots
|
||||
|
||||
|
||||
# Postprocess flow speed
|
||||
plotUxUpstream $timeDir $zMin
|
||||
plotUxMid $timeDir $zMin
|
||||
plotUxDownstream $timeDir $zMin
|
||||
|
||||
# Postprocess turbulence quantities
|
||||
if [ $baseEpsilonOrOmega == "epsilon" ]
|
||||
then
|
||||
items="epsilon_k_nut"
|
||||
|
||||
plotEpsilon $timeDir $items $zMin
|
||||
plotK $timeDir $items 3 $zMin
|
||||
plotMut $timeDir $items 4 $zMin
|
||||
|
||||
elif [ $baseEpsilonOrOmega == "omega" ]
|
||||
then
|
||||
items="k_nut_omega"
|
||||
|
||||
plotK $timeDir $items 2 $zMin
|
||||
plotMut $timeDir $items 3 $zMin
|
||||
plotOmega $timeDir $items $zMin
|
||||
|
||||
else
|
||||
echo "Chosen turbulence model is neither epsilon nor omega based." 1>&2
|
||||
exit 2
|
||||
fi
|
||||
|
||||
|
||||
#------------------------------------------------------------------------------
|
||||
@ -0,0 +1,111 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object blockMeshDict;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
scale 1;
|
||||
|
||||
// x = streamwise
|
||||
// y = spanwise
|
||||
// z = wall-normal
|
||||
|
||||
nx 500;
|
||||
ny 5;
|
||||
nz 50;
|
||||
xMin 0;
|
||||
xMax 5000.0;
|
||||
yMin 0;
|
||||
yMax 100.0;
|
||||
zMin 0.0;
|
||||
zMax 500.0;
|
||||
// blockMesh calculator input:
|
||||
// width of start cell = 1.0 (HW:p. 359)
|
||||
// number of cells = 50
|
||||
// total length = 500
|
||||
// blockMesh calculator output:
|
||||
// cell-to-cell expansion ratio = 1.076030437 (consistent with 1.076 (HW:Fig.1))
|
||||
zTotalExpansion 36.25795062;
|
||||
|
||||
vertices
|
||||
(
|
||||
($xMin $yMin $zMin)
|
||||
($xMax $yMin $zMin)
|
||||
($xMax $yMax $zMin)
|
||||
($xMin $yMax $zMin)
|
||||
($xMin $yMin $zMax)
|
||||
($xMax $yMin $zMax)
|
||||
($xMax $yMax $zMax)
|
||||
($xMin $yMax $zMax)
|
||||
);
|
||||
|
||||
blocks
|
||||
(
|
||||
hex (0 1 2 3 4 5 6 7) ($nx $ny $nz) simpleGrading (1 1 $zTotalExpansion)
|
||||
);
|
||||
|
||||
edges
|
||||
(
|
||||
);
|
||||
|
||||
boundary
|
||||
(
|
||||
inlet
|
||||
{
|
||||
type patch;
|
||||
faces
|
||||
(
|
||||
(0 4 7 3)
|
||||
);
|
||||
}
|
||||
ground
|
||||
{
|
||||
type wall;
|
||||
faces
|
||||
(
|
||||
(0 3 2 1)
|
||||
);
|
||||
}
|
||||
top
|
||||
{
|
||||
type patch;
|
||||
faces
|
||||
(
|
||||
(4 5 6 7)
|
||||
);
|
||||
}
|
||||
sides
|
||||
{
|
||||
type symmetry;
|
||||
faces
|
||||
(
|
||||
(1 5 4 0)
|
||||
(3 7 6 2)
|
||||
);
|
||||
}
|
||||
outlet
|
||||
{
|
||||
type patch;
|
||||
faces
|
||||
(
|
||||
(2 6 5 1)
|
||||
);
|
||||
}
|
||||
);
|
||||
|
||||
mergePatchPairs
|
||||
(
|
||||
);
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,62 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object controlDict;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
application simpleFoam;
|
||||
|
||||
startFrom latestTime;
|
||||
|
||||
startTime 0;
|
||||
|
||||
stopAt endTime;
|
||||
|
||||
endTime 5000;
|
||||
|
||||
deltaT 1;
|
||||
|
||||
writeControl timeStep;
|
||||
|
||||
writeInterval 500;
|
||||
|
||||
purgeWrite 0;
|
||||
|
||||
writeFormat ascii;
|
||||
|
||||
writePrecision 12;
|
||||
|
||||
writeCompression off;
|
||||
|
||||
timeFormat general;
|
||||
|
||||
timePrecision 6;
|
||||
|
||||
runTimeModifiable yes;
|
||||
|
||||
|
||||
functions
|
||||
{
|
||||
#include "sampleDict"
|
||||
|
||||
minMax
|
||||
{
|
||||
type fieldMinMax;
|
||||
libs (fieldFunctionObjects);
|
||||
writeControl writeTime;
|
||||
fields (U);
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,26 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object decomposeParDict;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
numberOfSubdomains 8;
|
||||
|
||||
method hierarchical;
|
||||
|
||||
coeffs
|
||||
{
|
||||
n (8 1 1);
|
||||
}
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,58 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object fvSchemes;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
ddtSchemes
|
||||
{
|
||||
default steadyState;
|
||||
}
|
||||
|
||||
gradSchemes
|
||||
{
|
||||
default Gauss linear;
|
||||
}
|
||||
|
||||
divSchemes
|
||||
{
|
||||
default none;
|
||||
div(phi,U) bounded Gauss linear;
|
||||
div(phi,epsilon) bounded Gauss limitedLinear 1;
|
||||
div(phi,omega) bounded Gauss limitedLinear 1;
|
||||
div(phi,k) bounded Gauss limitedLinear 1;
|
||||
div((nuEff*dev2(T(grad(U))))) Gauss linear;
|
||||
}
|
||||
|
||||
laplacianSchemes
|
||||
{
|
||||
default Gauss linear uncorrected;
|
||||
}
|
||||
|
||||
interpolationSchemes
|
||||
{
|
||||
default linear;
|
||||
}
|
||||
|
||||
snGradSchemes
|
||||
{
|
||||
default uncorrected;
|
||||
}
|
||||
|
||||
wallDist
|
||||
{
|
||||
method meshWave;
|
||||
}
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,59 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Website: www.openfoam.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
object fvSolution;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
solvers
|
||||
{
|
||||
p
|
||||
{
|
||||
solver GAMG;
|
||||
smoother GaussSeidel;
|
||||
tolerance 1e-8;
|
||||
relTol 0.01;
|
||||
}
|
||||
|
||||
"(U|k|epsilon|omega)"
|
||||
{
|
||||
solver smoothSolver;
|
||||
smoother GaussSeidel;
|
||||
tolerance 1e-8;
|
||||
relTol 0.01;
|
||||
}
|
||||
}
|
||||
|
||||
SIMPLE
|
||||
{
|
||||
nNonOrthogonalCorrectors 0;
|
||||
consistent true;
|
||||
pRefCell 0;
|
||||
pRefValue 0;
|
||||
}
|
||||
|
||||
relaxationFactors
|
||||
{
|
||||
equations
|
||||
{
|
||||
U 0.9;
|
||||
"(k|epsilon|omega)" 0.7;
|
||||
}
|
||||
}
|
||||
|
||||
cache
|
||||
{
|
||||
grad(U);
|
||||
}
|
||||
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -0,0 +1,79 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
| ========= | |
|
||||
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
|
||||
| \\ / O peration | Version: v1912 |
|
||||
| \\ / A nd | Web: www.OpenFOAM.com |
|
||||
| \\/ M anipulation | |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location system;
|
||||
object sampleDict;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
// The locations of the sample profiles correspond to:
|
||||
// Hargreaves-Wright (2007), Fig.6
|
||||
// DOI:10.1016/j.jweia.2006.08.002
|
||||
|
||||
samples
|
||||
{
|
||||
type sets;
|
||||
libs (sampling);
|
||||
setFormat raw;
|
||||
interpolationScheme cell;
|
||||
fields (U k epsilon nut omega);
|
||||
writeControl writeTime;
|
||||
|
||||
sets
|
||||
(
|
||||
x_0mPatch // inlet patch face centres
|
||||
{
|
||||
type face;
|
||||
axis z;
|
||||
start (0 50 0);
|
||||
end (0 50 500);
|
||||
}
|
||||
x_0mCell // inlet-first cell centres
|
||||
{
|
||||
type midPoint;
|
||||
axis z;
|
||||
start (5.0 50 0);
|
||||
end (5.0 50 500);
|
||||
}
|
||||
x_2500m
|
||||
{
|
||||
type face;
|
||||
axis z;
|
||||
start (2500 50 0);
|
||||
end (2500 50 500);
|
||||
}
|
||||
x_4000m
|
||||
{
|
||||
type face;
|
||||
axis z;
|
||||
start (4000 50 0);
|
||||
end (4000 50 500);
|
||||
}
|
||||
x_5000mCell // outlet patch face centres
|
||||
{
|
||||
type face;
|
||||
axis z;
|
||||
start (4995 50 0);
|
||||
end (4995 50 500);
|
||||
}
|
||||
x_5000mPatch // outlet-first cell centres
|
||||
{
|
||||
type face;
|
||||
axis z;
|
||||
start (5000 50 0);
|
||||
end (5000 50 500);
|
||||
}
|
||||
);
|
||||
}
|
||||
|
||||
|
||||
// *********************************************************************** //
|
||||
Reference in New Issue
Block a user