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7.91 kB
| cd "${0%/*}" || exit 1 # Run from this directory | |
| # Source tutorial run functions | |
| . "$WM_PROJECT_DIR/bin/tools/RunFunctions" | |
| # Get the serial/parallel mode | |
| ! isTest "$@" && [ -n "$1" ] && mode=$1 || mode=serial | |
| # Global variables | |
| SCALE=0.1 # Generated mesh is scaled by this factor | |
| TDC_CLEARANCE=4 | |
| # General calculation functions | |
| calc() | |
| { | |
| # Avoid locale problems with output of numbers from awk | |
| export LC_ALL=C | |
| # Default format | |
| _fmt="%.12f" | |
| # Custom format (optional): "int" returns an integer | |
| [ "$2" ] && \ | |
| case "$2" in | |
| int) _fmt="%.0f" ;; | |
| *) _fmt="$2" ;; | |
| esac | |
| awk "BEGIN{printf(\"$_fmt\", $1)}" | |
| } | |
| round() | |
| { | |
| # The 1.000001 factor makes 0.5 round up to 1 | |
| calc "$1*1.000001" int | |
| } | |
| # Create valve mesh at x = 0 | |
| createValveBaseMesh() | |
| { | |
| __mesh="$1" | |
| __valveLift="$2" | |
| __pistonPos="$3" | |
| # Mesh parameters | |
| _nCyl0=3 | |
| _nV0=3 | |
| _oneByDx=3 | |
| __nValve="$(calc "$_nV0 + $_oneByDx*$(round "$__valveLift")" int)" | |
| __nPiston="$(calc "$_nCyl0 + $_oneByDx*$(round "($__pistonPos - $__valveLift)")" int)" | |
| [ "$2" = "0" ] && __valveState=valveClosed || __valveState=valveOpen | |
| foamDictionary "system/blockMeshDict.$__valveState" -set "\ | |
| valveLift=-$__valveLift, \ | |
| nValve=$__nValve, \ | |
| pistonPos=-$__pistonPos, \ | |
| nPiston=$__nPiston" | |
| runApplication -a blockMesh -mesh "$__mesh" \ | |
| -dict "system/blockMeshDict.$__valveState" | |
| runApplication -a mirrorMesh -mesh "$__mesh" | |
| } | |
| # Offset in x-direction for a valve mesh | |
| valveOffset() | |
| { | |
| _dict="system/blockMeshDict.cylinder" | |
| _cylinderWidth="$(foamDictionary -entry cylinderWidth -value "$_dict")" | |
| _meshSecWidth="$(foamDictionary -entry meshSecWidth -value "$_dict")" | |
| _offset="$(calc "($_cylinderWidth - $_meshSecWidth) / 4.0")" | |
| case "$1" in | |
| exhaust) calc "-1.0*$_offset" ;; | |
| intake) echo "$_offset" ;; | |
| esac | |
| } | |
| # Create valve mesh at relevant x location, and correct patch names | |
| createValveMesh() | |
| { | |
| __mesh="$1" | |
| createValveBaseMesh "$__mesh" "$3" "$4" | |
| _type="$2" # intake or exhaust | |
| # Offset the mesh to in x-direction | |
| _offset="$(valveOffset "$_type")" | |
| runApplication -a transformPoints -mesh "$__mesh" "translate=($_offset 0 0)" | |
| # Correct patch names | |
| _boundary="constant/meshes/$__mesh/polyMesh/boundary" | |
| _valveName="$(echo "$_type" | cut -c1)v" # ev for exhaust, iv for intake | |
| _patchRenaming="\ | |
| entry0/valveHead=${_valveName}Head, \ | |
| entry0/valveStem=${_valveName}Stem, \ | |
| entry0/liner=nonCouple_${_valveName}_cyl" | |
| [ "$_type" = exhaust ] && \ | |
| _patchRenaming="$_patchRenaming, entry0/inlet=outlet" | |
| foamDictionary "$_boundary" -rename "$_patchRenaming" | |
| foamDictionary "$_boundary" \ | |
| -set entry0/nonCouple_"$_valveName"_cyl/type=patch | |
| foamDictionary "$_boundary" -remove \ | |
| -entry entry0/nonCouple_"$_valveName"_cyl/inGroups | |
| } | |
| # Create mesh for the cylinder in region around the valve meshes | |
| createCylinderMesh() | |
| { | |
| __mesh="$1" | |
| __pistonPos="$2" | |
| # Mesh parameters | |
| _nCyl0=3 | |
| _oneByDx=3 | |
| __nPiston="$(calc "$_nCyl0 + $_oneByDx*$(round "$__pistonPos")" int)" | |
| foamDictionary system/blockMeshDict.cylinder -set "\ | |
| pistonPos=-$__pistonPos, | |
| nPiston=$__nPiston" | |
| runApplication -a blockMesh -mesh "$__mesh" \ | |
| -dict system/blockMeshDict.cylinder | |
| } | |
| # Calculate the distance from the top of the piston to the end of the cylinder | |
| pistonPosition() | |
| { | |
| _crankAngleDeg=$1 | |
| _theta="$(calc "atan2(0, -1)*$_crankAngleDeg/180")" | |
| _conrod_m="$(foamDictionary constant/dynamicMeshDict -writePrecision 12 \ | |
| -entry mover/piston/motion/conRodLength -value)" | |
| _len="$(calc "$_conrod_m/$SCALE")" | |
| _stroke_m="$(foamDictionary constant/dynamicMeshDict -writePrecision 12 \ | |
| -entry mover/piston/motion/stroke -value)" | |
| _rad="$(calc "$_stroke_m/$SCALE/2")" | |
| _rST="$(calc "$_rad*sin($_theta)")" | |
| # r: position from the crank center | |
| _r="$(calc "$_rad*cos($_theta) + sqrt(($_len - $_rST)*($_len + $_rST))")" | |
| # Return piston position | |
| calc "$_len + $_rad - $_r + $TDC_CLEARANCE" | |
| } | |
| # Create valve and cylinder meshes and merge them | |
| # Separate the ports | |
| # Scale the mesh | |
| # Create fuel injection patch | |
| createMesh() | |
| { | |
| _mesh="$1" | |
| _pistonPos="$(pistonPosition "$_mesh")" | |
| # Create the mesh components | |
| createCylinderMesh "$_mesh" "$_pistonPos" | |
| createValveMesh _tmp_exhaust exhaust "$(evlift "$_mesh")" "$_pistonPos" | |
| createValveMesh _tmp_intake intake "$(ivlift "$_mesh")" "$_pistonPos" | |
| # Combine the mesh components | |
| runApplication -a mergeMeshes -mesh "$_mesh" \ | |
| -addMeshes '(_tmp_exhaust _tmp_intake)' | |
| # Delete temporary valve meshes | |
| rm -rf constant/meshes/_tmp* | |
| # Separate ports to mimic complicated engine assembly | |
| runApplication -a createBaffles -mesh "$_mesh" \ | |
| -dict system/createBafflesDict | |
| runApplication -a splitBaffles -mesh "$_mesh" | |
| runApplication -a transformPoints -mesh "$_mesh" \ | |
| "Rx=90, scale=($SCALE $SCALE $SCALE)" | |
| # Create fuel direct injection patch | |
| runApplication -a createPatch -mesh "$_mesh" -dict system/createPatchDict.inletFuel | |
| } | |
| # shellcheck disable=SC2086 | |
| createNCCs() | |
| { | |
| _meshOpt="" | |
| [ "$1" = constant ] || _meshOpt="-mesh $1" | |
| # Decompose (if necessary) and construct the non-conformal couplings that | |
| # connect the ports and enable the sliding interfaces | |
| case $mode in | |
| serial) | |
| runApplication -a createNonConformalCouples $_meshOpt \ | |
| -dict system/createNonConformalCouplesDict | |
| ;; | |
| parallel) | |
| runApplication -a decomposePar $_meshOpt -noFields | |
| runParallel -a createNonConformalCouples $_meshOpt \ | |
| -dict system/createNonConformalCouplesDict | |
| ;; | |
| *) | |
| echo "Error: mode $mode not recognised" | |
| exit 1 | |
| ;; | |
| esac | |
| } | |
| valvelift() | |
| { | |
| # Avoid locale problems with output of numbers from awk | |
| export LC_ALL=C | |
| # calculates valve lift as a triangular function of time | |
| # + _begin = begin time of upward slope | |
| # + _interval = time to triangle peak | |
| # + _start = lift value at start of slope | |
| # + _rate = rate of increase of lift | |
| # + _cur = current time | |
| _begin="$1" | |
| _interval="$2" | |
| _start="$3" | |
| _rate="$4" | |
| _mid="$(awk "BEGIN{printf(\"%.0f\", $_begin + $_interval)}")" | |
| _end="$(awk "BEGIN{printf(\"%.0f\", $_mid + $_interval)}")" | |
| _cur="$5" | |
| # Establish the "phase" of the triangular function | |
| _phase=0 | |
| for _t in $_begin $_mid $_end | |
| do | |
| [ "$(awk "BEGIN {print ($_cur >= $_t)}")" -eq 1 ] || continue | |
| _phase=$((_phase + 1)) | |
| done | |
| case $_phase in | |
| 0|3) echo 0 ;; | |
| 1) awk "BEGIN {print ($_start + $_rate*($_cur - $_begin))}" ;; | |
| 2) awk "BEGIN {print ($_start + $_rate*(2*$_mid - $_cur - $_begin))}" ;; | |
| esac | |
| } | |
| ivlift() | |
| { | |
| valvelift 340 140 0.1 0.02 "$1" | |
| } | |
| evlift() | |
| { | |
| valvelift 100 140 0.1 0.02 "$1" | |
| } | |
| times="0 \ | |
| 100 120 140 180 \ | |
| 200 220 \ | |
| 300 340 345 350 360 370 380 390 \ | |
| 410 440 460 \ | |
| 520 550 580 \ | |
| 600 610 620" | |
| # Generate meshes for all times | |
| for t in $times | |
| do | |
| echo "Generating mesh at time $t..." | |
| createMesh "$t" | |
| done | |
| # Copy the 0 polyMesh to constant | |
| cp -r constant/meshes/0/polyMesh constant/polyMesh | |
| # Generate non-conformal couples for all meshes | |
| for t in constant $times | |
| do | |
| echo "Generating non-conformal couples for mesh at time $t..." | |
| createNCCs "$t" | |
| done | |
| # Create the list of mesh times | |
| (cd constant/meshes && find -- * -maxdepth 0 | sort -n) > constant/meshTimes | |
| #------------------------------------------------------------------------------ | |