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"\n",
" function direction_cosine(vec1, vec2)\n",
" return dot(vec1,vec2) / (norm(vec1) * norm(vec2))\n",
" end\n",
"\n",
" function rotation_matrix(element_vector, x_axis, y_axis,z_axis)\n",
" # find the direction cosines\n",
" x_proj = direction_cosine(element_vector, x_axis)\n",
" y_proj = direction_cosine(element_vector, y_axis)\n",
" z_proj = direction_cosine(element_vector, z_axis);\n",
" return [[x_proj y_proj z_proj 0 0 0];[0 0 0 x_proj y_proj z_proj]]\n",
" end\n",
"\n",
" function rotation_matrix(element_vector, x_axis, y_axis,z_axis)\n",
" # find the direction cosines\n",
" L=norm(element_vector)\n",
" l = (element_vector[1])/L\n",
" m = (element_vector[2])/L\n",
" n = (element_vector[3])/L\n",
" D = ( l^2+ m^2+n^2)^0.5\n",
"\n",
" transMatrix=[[l m n 0 0 0 0 0 0 0 0 0];[-m/D l/D 0 0 0 0 0 0 0 0 0 0];[ -l*n/D -m*n/D D 0 0 0 0 0 0 0 0 0];[ 0 0 0 l m n 0 0 0 0 0 0];[ 0 0 0 -m/D l/D 0 0 0 0 0 0 0];[ 0 0 0 -l*n/D -m*n/D D 0 0 0 0 0 0];[ 0 0 0 0 0 0 l m n 0 0 0];[ 0 0 0 0 0 0 -m/D l/D 0 0 0 0];[ 0 0 0 0 0 0 -l*n/D -m*n/D D 0 0 0];[ 0 0 0 0 0 0 0 0 0 l m n];[ 0 0 0 0 0 0 0 0 0 -m/D l/D 0];[ 0 0 0 0 0 0 0 0 0 -l*n/D -m*n/D D]]\n",
"\n",
" return transMatrix\n",
" end\n",
" \n",
" #######################################################\n",
" function get_matrices(setup)\n",
"\n",
" nodes = setup[\"nodes\"]\n",
" edges = setup[\"edges\"]\n",
" ndofs = length(nodes)*6\n",
"\n",
" x_axis = [1 0 0]\n",
" y_axis = [0 1 0]\n",
" z_axis = [0 0 1]\n",
"\n",
" M = zeros((ndofs,ndofs))\n",
" K = zeros((ndofs,ndofs))\n",
" \n",
" \n",
" for edge in edges\n",
" #degrees_of_freedom = properties[\"degrees_of_freedom\"]\n",
"\n",
" element=parse(Int,edge[\"id\"][2:end])\n",
"\n",
" # find the nodes that the lements connects\n",
" fromNode = nodes[edge[\"source\"]+1]\n",
" toNode = nodes[edge[\"target\"]+1]\n",
" \n",
"\n",
" # the coordinates for each node\n",
" fromPoint = [fromNode[\"position\"][\"x\"]*15.0 fromNode[\"position\"][\"y\"]*15.0 fromNode[\"position\"][\"z\"]*15.0]\n",
" toPoint = [toNode[\"position\"][\"x\"]*15.0 toNode[\"position\"][\"y\"]*15.0 toNode[\"position\"][\"z\"]*15.0]\n",
"\n",
" # find the degrees of freedom for each node\n",
" dofs = convert(Array{Int}, fromNode[\"degrees_of_freedom\"])\n",
" dofs=vcat(dofs,convert(Array{Int}, toNode[\"degrees_of_freedom\"]))\n",
"\n",
" element_vector=toPoint-fromPoint\n",
"\n",
" # find element mass and stifness matrices\n",
" length = norm(element_vector)\n",
" rho = edge[\"density\"]\n",
" area = edge[\"area\"]\n",
" E = edge[\"stiffness\"]# youngs modulus\n",
"\n",
" A = edge[\"area\"]\n",
" G=1.0#todo shear_modulus\n",
" ixx = 1.0#todo section ixx\n",
" iyy = 1.0#todo section.iyy#\n",
" l0=length\n",
" j=1.0;#todo check\n",
" l02 = l0 * l0\n",
" l03 = l0 * l0 * l0\n",
" \n",
" # find element mass and stifness matrices\n",
" length = norm(element_vector)\n",
" rho = edge[\"density\"]\n",
" area = edge[\"area\"]\n",
" E = edge[\"stiffness\"]# youngs modulus\n",
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" \n",
" \n",
" \n",
" A = edge[\"area\"]\n",
" G=1.0#todo shear_modulus\n",
" ixx = 1.0#todo section ixx\n",
" iyy = 1.0#todo section.iyy#\n",
" j=1.0;#todo check\n",
" \n",
" \n",
" h = 2.38 # mm\n",
" b = 2.38 # mm\n",
" E = 2000 # MPa\n",
" rho = 7.85e-9 / 3 # kg/mm^3\n",
" G = E * 1 / 3 # MPa\n",
" A=h*b\n",
" Q = 1 / 3 - 0.2244 / (min(h / b, b / h) + 0.1607)\n",
" J = Q * min(h * b^3, b * h^3)\n",
" I= b*h^3/12\n",
" ixx=I\n",
" iyy=I\n",
" j=J\n",
" \n",
" l0=length\n",
" l02 = l0 * l0\n",
" l03 = l0 * l0 * l0\n",
"\n",
" # Cm = rho * area * length /6.0\n",
" # Ck= E * area / length \n",
"\n",
" # m = [[2 1];[1 2]]\n",
" # k = [[1 -1];[-1 1]]\n",
"\n",
" k = [[E*A/l0 0 0 0 0 0 -E*A/l0 0 0 0 0 0];[0 12*E*ixx/l03 0 0 0 6*E*ixx/l02 0 -12*E*ixx/l03 0 0 0 6*E*ixx/l02];[0 0 12*E*iyy/l03 0 -6*E*iyy/l02 0 0 0 -12*E*iyy/l03 0 -6*E*iyy/l02 0];[0 0 0 G*j/l0 0 0 0 0 0 -G*j/l0 0 0];[0 0 -6*E*iyy/l02 0 4*E*iyy/l0 0 0 0 6*E*iyy/l02 0 2*E*iyy/l0 0];[0 6*E*ixx/l02 0 0 0 4*E*ixx/l0 0 -6*E*ixx/l02 0 0 0 2*E*ixx/l0];[-E*A/l0 0 0 0 0 0 E*A/l0 0 0 0 0 0];[0 -12*E*ixx/l03 0 0 0 -6*E*ixx/l02 0 12*E*ixx/l03 0 0 0 -6*E*ixx/l02];[0 0 -12*E*iyy/l03 0 6*E*iyy/l02 0 0 0 12*E*iyy/l03 0 6*E*iyy/l02 0];[0 0 0 -G*j/l0 0 0 0 0 0 G*j/l0 0 0];[0 0 -6*E*iyy/l02 0 2*E*iyy/l0 0 0 0 6*E*iyy/l02 0 4*E*iyy/l0 0];[0 6*E*ixx/l02 0 0 0 2*E*ixx/l0 0 -6*E*ixx/l02 0 0 0 4*E*ixx/l0]]\n",
"\n",
" \n",
" ################################\n",
"# mass=10\n",
"# nu=0.35\n",
"# W = 75\n",
"# L = W/sqrt(2)\n",
"# L=length\n",
"# n_min = 1\n",
"# n_max = 7\n",
"# # Cross Section inputs, must be floats\n",
"# E = 2000 # MPa\n",
"# G = E * 1 / 3 # MPa\n",
"# h = 2.38 # mm\n",
"# b = 2.38 # mm\n",
"# rho = 7.85e-9 / 3 # kg/mm^3\n",
"# S = h * b\n",
"# Sy = (S * (6 + 12 * nu + 6 * nu^2)/ (7 + 12 * nu + 4 * nu^2))\n",
"# # For solid rectangular cross section (width=b, depth=d & ( b < d )):\n",
"# Q = 1 / 3 - 0.2244 / (min(h / b, b / h) + 0.1607)\n",
"# J = Q * min(h * b^3, b * h^3)\n",
" \n",
" \n",
"# ##if voxels\n",
"# #nu=0\n",
"# #L=l\n",
"# #a1 = E*L # EA/L : Units of N/m\n",
"# #a2 = E * L*L*L / (12.0*(1+nu)) # GJ/L : Units of N-m\n",
"# #b1 = E*L # 12EI/L^3 : Units of N/m\n",
"# #b2 = E*L*L/2.0 # 6EI/L^2 : Units of N (or N-m/m: torque related to linear distance)\n",
"# #b3 = E*L*L*L/6.0 # 2EI/L : Units of N-m\n",
" \n",
"# I= b*h^3/12\n",
"# # J=b*h*(b*b+h*h)/12\n",
"# a1=E*b*h/L\n",
"# a2=G*J/L\n",
"# b1=12*E*I/(L^3)\n",
"# b2=6*E*I/(L^2)\n",
"# b3=2*E*I/(L)\n",
"\n",
" \n",
"\n",
"# k = [[E*A/l0 0 0 0 0 0 -E*A/l0 0 0 0 0 0];[0 12*E*ixx/l03 0 0 0 6*E*ixx/l02 0 -12*E*ixx/l03 0 0 0 6*E*ixx/l02];[0 0 12*E*iyy/l03 0 -6*E*iyy/l02 0 0 0 -12*E*iyy/l03 0 -6*E*iyy/l02 0];[0 0 0 G*j/l0 0 0 0 0 0 -G*j/l0 0 0];[0 0 -6*E*iyy/l02 0 4*E*iyy/l0 0 0 0 6*E*iyy/l02 0 2*E*iyy/l0 0];[0 6*E*ixx/l02 0 0 0 4*E*ixx/l0 0 -6*E*ixx/l02 0 0 0 2*E*ixx/l0];[-E*A/l0 0 0 0 0 0 E*A/l0 0 0 0 0 0];[0 -12*E*ixx/l03 0 0 0 -6*E*ixx/l02 0 12*E*ixx/l03 0 0 0 -6*E*ixx/l02];[0 0 -12*E*iyy/l03 0 6*E*iyy/l02 0 0 0 12*E*iyy/l03 0 6*E*iyy/l02 0];[0 0 0 -G*j/l0 0 0 0 0 0 G*j/l0 0 0];[0 0 -6*E*iyy/l02 0 2*E*iyy/l0 0 0 0 6*E*iyy/l02 0 4*E*iyy/l0 0];[0 6*E*ixx/l02 0 0 0 2*E*ixx/l0 0 -6*E*ixx/l02 0 0 0 4*E*ixx/l0]]\n",
"# k= [[ a1 0 0 0 0 0 -a1 0 0 0 0 0 ];\n",
"# [ 0 b1 0 0 0 b2 0 -b1 0 0 0 b2 ];\n",
"# [ 0 0 b1 0 -b2 0 0 0 -b1 0 -b2 0 ];\n",
"# [ 0 0 0 a2 0 0 0 0 0 -a2 0 0 ];\n",
"# [ 0 0 0 0 2b3 0 0 0 b2 0 b3 0 ];\n",
"# [ 0 0 0 0 0 2b3 0 -b2 0 0 0 b3 ];\n",
"# [ 0 0 0 0 0 0 a1 0 0 0 0 0 ];\n",
"# [ 0 0 0 0 0 0 0 b1 0 0 0 -b2 ];\n",
"# [ 0 0 0 0 0 0 0 0 b1 0 b2 0 ];\n",
"# [ 0 0 0 0 0 0 0 0 0 a2 0 0 ];\n",
"# [ 0 0 0 0 0 0 0 0 0 0 2b3 0 ];\n",
"# [ 0 0 0 0 0 0 0 0 0 0 0 2b3 ]]\n",
" # find rotated mass and stifness matrices\n",
" tau = rotation_matrix(element_vector, x_axis,y_axis,z_axis)\n",
"\n",
" # m_r=transpose(tau)*m*tau\n",
" k_r=transpose(tau)*k*tau\n",
"\n",
" # change from element to global coordinate\n",
" index= dofs.+1\n",
"\n",
" B=zeros((12,ndofs))\n",
" for i in 1:12\n",
" B[i,index[i]]=1.0\n",
" end\n",
"\n",
"\n",
" # M_rG= transpose(B)*m_r*B\n",
" K_rG= transpose(B)*k_r*B\n",
"\n",
" # M += Cm .* M_rG\n",
" # K += Ck .* K_rG\n",
" K += K_rG\n",
"\n",
" end\n",
" \n",
" \n",
" # construct the force vector\n",
" F=zeros(ndofs)\n",
" remove_indices=[];\n",
" for node in nodes\n",
" #insert!(F,i, value);\n",
" #F=vcat(F,value)\n",
" \n",
" \n",
" i=parse(Int,node[\"id\"][2:end])\n",
" f=node[\"force\"]\n",
" \n",
" # println(f)\n",
" F[(i)*6+1]+=f[\"x\"]\n",
" F[(i)*6+2]+=f[\"y\"]\n",
" F[(i)*6+3]+=f[\"z\"]\n",
" F[(i)*6+4]+=0\n",
" F[(i)*6+5]+=0\n",
" F[(i)*6+6]+=0\n",
" Load+=f[\"y\"]\n",
" if (F[(i)*6+2]!=0)\n",
" append!(topNodesIndices,i+1)\n",
" end\n",
" \n",
" dofs = convert(Array{Int}, node[\"degrees_of_freedom\"]).+1\n",
" restrained_dofs=node[\"restrained_degrees_of_freedom\"]\n",
" for (index, value) in enumerate(dofs)\n",
" if restrained_dofs[index]\n",
" append!( remove_indices, value)\n",
" end\n",
" end\n",
" \n",
" end\n",
"\n",
" #println(remove_indices)\n",
" #print(K)\n",
" #print(F)\n",
" \n",
"\n",
" #M = M[setdiff(1:end, remove_indices), :]\n",
" K = K[setdiff(1:end, remove_indices), :]\n",
"\n",
" #M = M[:,setdiff(1:end, remove_indices)]\n",
" K = K[:,setdiff(1:end, remove_indices)]\n",
"\n",
" F = F[setdiff(1:end, remove_indices)]\n",
" \n",
" U=zeros(ndofs)\n",
" \n",
" return M,K,F,U,remove_indices\n",
" end\n",
"\n",
" \n",
" function updateDisplacement(setup, X)\n",
" nodes= setup[\"nodes\"]\n",
" i=0\n",
" for node in nodes\n",
" \n",
"# if !node[\"restrained_degrees_of_freedom\"][2]\n",
" #i=parse(Int,node[\"id\"][2:end])\n",
" node[\"displacement\"][\"x\"]=X[(i)*6+1]/15\n",
" node[\"displacement\"][\"y\"]=X[(i)*6+2]/15\n",
" node[\"displacement\"][\"z\"]=X[(i)*6+3]/15\n",
" node[\"angle\"][\"x\"]=X[(i)*6+4]\n",
" node[\"angle\"][\"y\"]=X[(i)*6+5]\n",
" node[\"angle\"][\"z\"]=X[(i)*6+6]\n",
" append!(displacementFEA,[Vector3(X[(i)*6+1],X[(i)*6+2],X[(i)*6+3])])\n",
" i=i+1\n",
"# else\n",
"# append!(displacementFEA,[Vector3(0,0,0)])\n",
"# end\n",
" end\n",
" end\n",
" \n",
" #######################################################\n",
"\n",
" function get_stresses(setup)\n",
" nodes = setup[\"nodes\"]\n",
" edges = setup[\"edges\"]\n",
" ndofs = length(nodes)*6\n",
"\n",
" x_axis = [1 0 0]\n",
" y_axis = [0 1 0]\n",
" z_axis = [0 0 1]\n",
"\n",
" # find the stresses in each member\n",
" stresses=zeros(length(edges))\n",
" max11=-10e6\n",
" min11=10e6\n",
" for edge in edges\n",
" #degrees_of_freedom = properties[\"degrees_of_freedom\"]\n",
"\n",
" element=parse(Int,edge[\"id\"][2:end])\n",
"\n",
" # find the nodes that the lements connects\n",
" fromNode = nodes[edge[\"source\"]+1]\n",
" toNode = nodes[edge[\"target\"]+1]\n",
"\n",
" # the coordinates for each node\n",
" fromPoint = [fromNode[\"position\"][\"x\"]*15.0 fromNode[\"position\"][\"y\"]*15.0 fromNode[\"position\"][\"z\"]*15.0]\n",
" toPoint = [toNode[\"position\"][\"x\"]*15.0 toNode[\"position\"][\"y\"]*15.0 toNode[\"position\"][\"z\"]*15.0]\n",
"\n",
" # find the degrees of freedom for each node\n",
" dofs = convert(Array{Int}, fromNode[\"degrees_of_freedom\"])\n",
" dofs=vcat(dofs,convert(Array{Int}, toNode[\"degrees_of_freedom\"]))\n",
"\n",
" element_vector=toPoint-fromPoint\n",
"\n",
"\n",
" # find rotated mass and stifness matrices\n",
" tau = rotation_matrix(element_vector, x_axis,y_axis,z_axis)\n",
"\n",
" # i1=parse(Int,fromNode[\"id\"][2:end])\n",
" # i2=parse(Int,toNode[\"id\"][2:end])\n",
"\n",
" # global_displacements=[X[(i1)*6+1] X[(i1)*6+2] X[(i1)*6+3] X[(i1)*6+4] X[(i1)*6+5] X[(i1)*6+6] X[(i2)*6+1] X[(i2)*6+2] X[(i2)*6+3] X[(i2)*6+4] X[(i2)*6+5] X[(i2)*6+6]] # todo change\n",
" global_displacements=[fromNode[\"displacement\"][\"x\"]*15 fromNode[\"displacement\"][\"y\"]*15 fromNode[\"displacement\"][\"z\"]*15 fromNode[\"angle\"][\"x\"] fromNode[\"angle\"][\"y\"] fromNode[\"angle\"][\"z\"] toNode[\"displacement\"][\"x\"]*15 toNode[\"displacement\"][\"y\"]*15 toNode[\"displacement\"][\"z\"]*15 toNode[\"angle\"][\"x\"] toNode[\"angle\"][\"y\"] toNode[\"angle\"][\"z\"]] # todo change\n",
"\n",
" # nodal displacement\n",
"\n",
" q=tau*transpose(global_displacements)\n",
" # println(q)\n",
" # calculate the strain and stresses\n",
" strain =(q[7]-q[1])/norm(element_vector)\n",
" E = edge[\"stiffness\"]# youngs modulus\n",
" E=2000\n",
" stress=E.*strain\n",
" edge[\"stress\"]=stress\n",
" if stress>max11\n",
" max11=stress\n",
" end\n",
" if stress<min11\n",
" min11=stress\n",
" end\n",
" # println(element)\n",
" # println(stress)\n",
" end\n",
"\n",
"\n",
"\n",
" setup[\"viz\"][\"minStress\"]=min11\n",
" setup[\"viz\"][\"maxStress\"]=max11\n",
" return stresses\n",
" end\n",
" \n",
" function initialize(setup)\n",
" nodes = setup[\"nodes\"]\n",
" ndofs = length(nodes)*6\n",
" \n",
" i=0\n",
" for node in nodes\n",
" dg=[]\n",
" for ii in 0:5\n",
" append!(dg,i+ii) \n",
" end\n",
" i+=6\n",
" node[\"degrees_of_freedom\"]=dg\n",
" end\n",
" end\n",
"\n",
" #######################################################\n",
" function solveFea(setup)\n",
" // # determine the global matrices\n",
" initialize(setup)\n",
" \n",
" M,K,F,U,ind=get_matrices(setup)\n",
" \n",
" #println(M)\n",
" #println(K)\n",
" #println(F)\n",
"\n",
" #evals=eigvals(K,M)\n",
" #evecs=eigvecs(K,M)\n",
" #frequencies=sqrt.(evals)\n",
" X=inv(K)*F\n",
" U[setdiff(1:end, ind)]=X\n",
"\n",
" updateDisplacement(setup, U)\n",
"\n",
" # determine the stresses in each element\n",
" stresses=get_stresses(setup)\n",
" end\n",
" #######################################################\n",
" displacementFEA=[]\n",
" Load=0\n",
" topNodesIndices=[]\n",
" solveFea(setup)\n",
" return displacementFEA,Load,topNodesIndices\n",
"end"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"data": {
"text/plain": [
"getYoungsModulus (generic function with 1 method)"
]
},
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"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"function getYoungsModulus(latticeSize,voxelSize,disp,Load,topNodesIndices)\n",
" F=-Load\n",
" l0=voxelSize*latticeSize\n",
" A=l0*l0\n",
"\n",
" δl1=-mean( x.y for x in disp[topNodesIndices])\n",
" \n",
" stresses=F/A\n",
" strain=δl1/l0\n",
" println(\"Load=$Load\")\n",
" println(\"stress=$stresses\")\n",
"\n",
" E=stresses/strain \n",
"\n",
" return E\n",
"end\n"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"data": {
"text/plain": [
"getSetup (generic function with 1 method)"
]
},
"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"function getSetup(latticeSize)\n",
" setup = Dict()\n",
" name=string(\"../../json/setupTestUni$latticeSize\",\".json\")\n",
"# name=string(\"../../json/canteliver\",\".json\")\n",
" \n",
"# open(\"../../json/setupValid2.json\", \"r\") do f\n",
"# open(\"../../json/setupTest.json\", \"r\") do f\n",
" # open(\"../../json/trialJulia.json\", \"r\") do f\n",
"# open(\"../../json/setupTestUni4.json\", \"r\") do f\n",
" # open(\"../../json/setupChiral.json\", \"r\") do f\n",
"# open(\"../../json/setupTestCubeUni10.json\", \"r\") do f\n",
" open(name, \"r\") do f\n",
"# global setup\n",
" dicttxt = String(read(f)) # file information to string\n",
" setup=JSON.parse(dicttxt) # parse and transform data\n",
" end\n",
"\n",
" setup=setup[\"setup\"]\n",
" return setup\n",
"end"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"name": "stdout",
"output_type": "stream",
"text": [
"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"setup=getSetup(latticeSize)\n",
"displacementFEA,Load,topNodesIndices=fea(setup)\n",
"topNodesIndices\n",
"println(length(setup[\"nodes\"]))\n",
"length(setup[\"edges\"])"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"data": {
"text/plain": [
"5-element Array{Float64,1}:\n",
" 0.0\n",
" 0.0\n",
" 0.0\n",
" 0.0\n",
" 0.0"
]
},
"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"DDisplacements=[[],[],[],[],[]]\n",
"DDisplacementsFEA=[[],[],[],[],[]]\n",
"Loads=[0.0,0,0,0,0]\n",
"EsFEA=[0.0,0,0,0,0]\n",
"Es=[0.0,0,0,0,0]"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"data": {
"text/plain": [
"Dict{String,Any} with 8 entries:\n",
" \"nodes\" => Any[Dict{String,Any}(\"degrees_of_freedom\"=>Any[0, 1, 2, 3, …\n",
" \"voxelSize\" => 5\n",
" \"numTimeSteps\" => 100\n",
" \"hierarchical\" => false\n",
" \"animation\" => Dict{String,Any}(\"exaggeration\"=>2000,\"speed\"=>3,\"showDispl…\n",
" \"viz\" => Dict{String,Any}(\"colorMap\"=>0,\"exaggeration\"=>10000,\"color…\n",
" \"edges\" => Any[Dict{String,Any}(\"source\"=>0,\"area\"=>1,\"density\"=>0.028…\n",
"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"setup"
]
},
{
"cell_type": "code",
"metadata": {},
"outputs": [
{
"data": {
"text/plain": [
"metadata": {},
"output_type": "execute_result"
}
],
"source": [
"setup=getSetup(latticeSize)\n",
"displacementFEA,Load,topNodesIndices=fea(setup)\n",
"# displacementFEA,Load,topNodesIndices=feaDisplacement(setup,latticeSize)\n",
"updateDataAndSaveFEA!(setup,\"../../json/trialJuliaParallelGPU.json\")\n"
"metadata": {},
"outputs": [
{
"name": "stdout",
"output_type": "stream",
"text": [
"dt: 0.007294855212986816\n",
"first timestep took 0.000645101 seconds\n",
"ran latticeSize 3 with 144 voxels and 432 edges for 6000 time steps took 2.0397974 seconds\n",
"Load=-900.0\n",
"stress=0.017777777777777778\n",
"Load=-900.0\n",
"stress=0.017777777777777778\n",
"EsFEA:[0.0, 1.3631163779051199, 1.4928557096014121, 0.0, 0.0]\n",
"Es:[0.0, 1.3636389591522067, 1.4821324986526747, 0.0, 0.0]\n",
"FEA displacement= -3.161875031059339,converged displacement= -3.199251807603066\n"
]
},
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],
"source": [
"\n",
"setup=getSetup(latticeSize)\n",
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"displacements=[]\n",
"save=true\n",
"returnEvery=10\n",
"runMetavoxelGPU!(setup,numTimeSteps,latticeSize,displacements,returnEvery,true)\n",
"\n",
"numTimeStepsRecorded=length(displacements)\n",
"d=[]\n",
"dFEA=[]\n",
"j=length(displacements[end])\n",
"step=100\n",
"for i in 1:step:numTimeStepsRecorded\n",
" append!(d,displacements[i][j].y)\n",
" append!(dFEA,displacementFEA[j].y)\n",
"end\n",
"Loads[latticeSize]=Load\n",
"DDisplacements[latticeSize]=d\n",
"DDisplacementsFEA[latticeSize]=dFEA\n",
"\n",
"E1=getYoungsModulus(latticeSize,75,displacementFEA,Load,topNodesIndices)\n",
"E2=getYoungsModulus(latticeSize,75,displacements[end],Load,topNodesIndices)\n",
"\n",
"EsFEA[latticeSize]=E1\n",
"Es[latticeSize]=E2\n",
"\n",
"print(\"EsFEA:\" )\n",
"println(EsFEA)\n",
"print(\"Es:\" )\n",
"println(Es)\n",
"\n",
"println(\"FEA displacement= $(displacementFEA[j].y),converged displacement= $(displacements[numTimeStepsRecorded][j].y)\")\n",
"plot(1:step:numTimeStepsRecorded,d,label=\"Dynamic\",xlabel=\"timestep\",ylabel=\"displacement\",title=\"$latticeSize Voxel Convergence Study\")\n",
"plot!(1:step:numTimeStepsRecorded,dFEA,label=\"FEA\")\n",
"# savefig(\"4_voxel_convergence\")\n"
]
},
{
"cell_type": "code",
"metadata": {},
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