functionObjects: Added patchCutLayerAverage
This function object writes graphs of patch face values, area-averaged in
planes perpendicular to a given direction. It adaptively grades the
distribution of graph points to match the resolution of the mesh.
Example of function object specification:
patchCutLayerAverage1
{
type patchCutLayerAverage;
libs ("libpatchCutLayerAverageFunctionObject.so");
writeControl writeTime;
writeInterval 1;
patch lowerWall;
direction (1 0 0);
nPoints 100;
interpolate no;
fields (p U);
axis x;
setFormat raw;
}
A packaged function object is also included, which permits the following
syntax to be used, either with #includeFunc in the system/controlDict,
or with the -func option to foamPostProcess:
graphPatchCutLayerAverage
(
funcName=aerofoilLowerPressure,
patch=aerofoilLower,
direction=(0.15 -0.016 0),
nPoints=100,
p
)
This commit is contained in:
Will Bainbridge
@ -220,13 +220,30 @@ boundary
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(27 28 57 56)
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);
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}
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hydrofoil
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hydrofoilTip
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{
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type wall;
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inGroups (hydrofoil);
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faces
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(
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(12 13 42 41)
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);
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}
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hydrofoilLower
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{
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type wall;
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inGroups (hydrofoil);
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faces
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(
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(12 16 45 41)
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);
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}
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hydrofoilUpper
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{
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type wall;
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inGroups (hydrofoil);
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faces
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(
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(13 16 45 42)
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);
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}
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@ -54,9 +54,50 @@ maxDeltaT 1e-4;
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functions
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{
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#includeFunc yPlus(phase=liquid)
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#includeFunc cellMin(funcName=min, alpha.liquid, alpha.gas, p, p_rgh, U.liquid, U.gas, T.gas, T.liquid)
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#includeFunc cellMax(funcName=max, alpha.liquid, alpha.gas, p, p_rgh, U.liquid, U.gas, T.gas, T.liquid)
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#includeFunc hydrofoilPressure
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#includeFunc cellMin
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(
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funcName=min,
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alpha.liquid,
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alpha.gas,
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p,
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p_rgh,
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U.liquid,
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U.gas,
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T.gas,
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T.liquid
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)
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#includeFunc cellMax
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(
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funcName=max,
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alpha.liquid,
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alpha.gas,
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p,
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p_rgh,
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U.liquid,
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U.gas,
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T.gas,
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T.liquid
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)
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#includeFunc graphPatchCutLayerAverage
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(
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funcName=hydrofoilLowerPressure,
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patch=hydrofoilLower,
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direction=(0.15 -0.016 0),
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nPoints=100,
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p
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)
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#includeFunc graphPatchCutLayerAverage
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(
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funcName=hydrofoilUpperPressure,
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patch=hydrofoilUpper,
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direction=(0.15 -0.016 0),
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nPoints=100,
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p
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)
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}
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@ -1,149 +0,0 @@
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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 | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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type sets;
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libs ("libsampling.so");
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writeControl writeTime;
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interpolationScheme cellPoint;
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setFormat raw;
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fields (p);
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axis xyz;
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sets
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(
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lower
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{
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type boundaryPoints;
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axis xyz;
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points
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(
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(0 0 0)
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(0.003 -0.0003 0)
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(0.006 -0.0006 0)
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(0.009 -0.0009 0)
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(0.012 -0.0012 0)
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(0.015 -0.0015 0)
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(0.018 -0.0018 0)
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(0.021 -0.0021 0)
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(0.024 -0.0024 0)
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(0.027 -0.0027 0)
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(0.03 -0.003 0)
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(0.033 -0.0033 0)
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(0.036 -0.0036 0)
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(0.039 -0.0039 0)
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(0.042 -0.0042 0)
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(0.045 -0.0045 0)
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(0.048 -0.0048 0)
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(0.051 -0.0051 0)
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(0.054 -0.0054 0)
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(0.057 -0.0057 0)
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(0.06 -0.006 0)
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(0.063 -0.0063 0)
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(0.066 -0.0066 0)
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(0.069 -0.0069 0)
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(0.072 -0.0072 0)
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(0.075 -0.0075 0)
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(0.078 -0.0078 0)
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(0.081 -0.0081 0)
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(0.084 -0.0084 0)
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(0.087 -0.0087 0)
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(0.09 -0.009 0)
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(0.093 -0.0093 0)
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(0.096 -0.0096 0)
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(0.099 -0.0099 0)
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(0.102 -0.0102 0)
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(0.105 -0.0105 0)
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(0.108 -0.0108 0)
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(0.111 -0.0111 0)
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(0.114 -0.0114 0)
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(0.117 -0.0117 0)
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(0.12 -0.012 0)
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(0.123 -0.0123 0)
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(0.126 -0.0126 0)
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(0.129 -0.0129 0)
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(0.132 -0.0132 0)
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(0.135 -0.0135 0)
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(0.138 -0.0138 0)
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(0.141 -0.0141 0)
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(0.144 -0.0144 0)
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(0.147 -0.0147 0)
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(0.15 -0.015 0)
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);
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patches (hydrofoil);
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maxDistance 1;
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}
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upper
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{
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type boundaryPoints;
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axis xyz;
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points
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(
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(0 0.015 0)
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(0.003 0.0147 0)
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(0.006 0.0144 0)
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(0.009 0.0141 0)
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(0.012 0.0138 0)
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(0.015 0.0135 0)
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(0.018 0.0132 0)
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(0.021 0.0129 0)
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(0.024 0.0126 0)
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(0.027 0.0123 0)
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(0.03 0.012 0)
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(0.033 0.0117 0)
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(0.036 0.0114 0)
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(0.039 0.0111 0)
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(0.042 0.0108 0)
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(0.045 0.0105 0)
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(0.048 0.0102 0)
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(0.051 0.0099 0)
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(0.054 0.0096 0)
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(0.057 0.0093 0)
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(0.06 0.009 0)
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(0.063 0.0087 0)
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(0.066 0.0084 0)
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(0.069 0.0081 0)
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(0.072 0.0078 0)
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(0.075 0.0075 0)
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(0.078 0.0072 0)
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(0.081 0.0069 0)
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(0.084 0.0066 0)
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(0.087 0.0063 0)
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(0.09 0.006 0)
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(0.093 0.0057 0)
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(0.096 0.0054 0)
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(0.099 0.0051 0)
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(0.102 0.0048 0)
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(0.105 0.0045 0)
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(0.108 0.0042 0)
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(0.111 0.0039 0)
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(0.114 0.0036 0)
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(0.117 0.0033 0)
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(0.12 0.003 0)
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(0.123 0.0027 0)
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(0.126 0.0024 0)
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(0.129 0.0021 0)
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(0.132 0.0018 0)
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(0.135 0.0015 0)
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(0.138 0.0012 0)
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(0.141 0.0009 0)
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(0.144 0.0006 0)
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(0.147 0.0003 0)
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(0.15 0 0)
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);
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patches (hydrofoil);
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maxDistance 1;
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}
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);
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// ************************************************************************* //
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@ -6,8 +6,8 @@ then
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exit 1
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fi
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lowerFile=postProcessing/hydrofoilPressure/$(foamListTimes -latestTime)/lower.xy
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upperFile=postProcessing/hydrofoilPressure/$(foamListTimes -latestTime)/upper.xy
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lowerFile=postProcessing/hydrofoilLowerPressure/$(foamListTimes -latestTime)/patchCutLayerAverage.xy
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upperFile=postProcessing/hydrofoilUpperPressure/$(foamListTimes -latestTime)/patchCutLayerAverage.xy
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gnuplot<<EOF
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@ -38,8 +38,8 @@ rhoInf = 998.4
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set xlabel 'x/L'
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set ylabel 'Cp'
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plot [0:1] \
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'$lowerFile' u (\$1/0.15):(2*(\$4-pInf)/(rhoInf*UInf*UInf)) w l lt 1 t 'Simulation Lower', \
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'$upperFile' u (\$1/0.15):(2*(\$4-pInf)/(rhoInf*UInf*UInf)) w l lt 2 t 'Simulation Upper', \
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'$lowerFile' u (\$2/0.15):(2*(\$6-pInf)/(rhoInf*UInf*UInf)) w l lt 1 t 'Simulation Lower', \
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'$upperFile' u (\$2/0.15):(2*(\$6-pInf)/(rhoInf*UInf*UInf)) w l lt 2 t 'Simulation Upper', \
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'\$experiment' u 1:2 w p lt rgb "black" pt 4 t 'Experiment'
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EOF
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Reference in New Issue
Block a user