FEM: stress and strain components, use more comon order and notation
This commit is contained in:
committed by
Yorik van Havre
parent
194a68001d
commit
86dc590a8a
@@ -425,7 +425,10 @@ def read_frd_result(frd_input):
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stress_4 = float(line[49:61])
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stress_5 = float(line[61:73])
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stress_6 = float(line[73:85])
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mode_stress[elem] = (stress_1, stress_2, stress_3, stress_4, stress_5, stress_6)
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# CalculiX frd files: (Sxx, Syy, Szz, Sxy, Syz, Szx)
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# FreeCAD: (Sxx, Syy, Szz, Sxy, Sxz, Syz)
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# thus exchange the last two entries
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mode_stress[elem] = (stress_1, stress_2, stress_3, stress_4, stress_6, stress_5)
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# Check if we found strain section
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if line[5:13] == "TOSTRAIN":
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@@ -439,7 +442,10 @@ def read_frd_result(frd_input):
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strain_4 = float(line[49:61])
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strain_5 = float(line[61:73])
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strain_6 = float(line[73:85])
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mode_strain[elem] = (strain_1, strain_2, strain_3, strain_4, strain_5, strain_6)
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# CalculiX frd files: (Exx, Eyy, Ezz, Exy, Eyz, Ezx)
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# FreeCAD: (Exx, Eyy, Ezz, Exy, Exz, Eyz)
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# thus exchange the last two entries
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mode_strain[elem] = (strain_1, strain_2, strain_3, strain_4, strain_6, strain_5)
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# Check if we found an equivalent plastic strain section
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if line[5:7] == "PE":
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@@ -349,8 +349,8 @@ def calculate_von_mises(i):
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s22 = i[1]
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s33 = i[2]
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s12 = i[3]
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s23 = i[4]
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s31 = i[5]
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s31 = i[4]
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s23 = i[5]
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s11s22 = pow(s11 - s22, 2)
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s22s33 = pow(s22 - s33, 2)
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s33s11 = pow(s33 - s11, 2)
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@@ -360,9 +360,9 @@ def calculate_von_mises(i):
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def calculate_principal_stress(i):
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sigma = np.array([[i[0], i[3], i[5]],
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[i[3], i[1], i[4]],
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[i[5], i[4], i[2]]]) # https://forum.freecadweb.org/viewtopic.php?f=18&t=24637&start=10#p240408
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sigma = np.array([[i[0], i[3], i[4]],
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[i[3], i[1], i[5]],
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[i[4], i[5], i[2]]]) # https://forum.freecadweb.org/viewtopic.php?f=18&t=24637&start=10#p240408
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try: # it will fail if NaN is inside the array,
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# compute principal stresses
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