import abdbeam as ab sc = ab.Section() # Create a materials dictionary: mts = dict() mts[1] = ab.Laminate() ply_mat = ab.PlyMaterial(0.166666, 148000, 9650, 4550, 0.3) mts[1].ply_materials[1] = ply_mat mts[1].plies = [[0, 1]] * 6 + [[45, 1]] * 6 # Create a points dictionary based on Y and Z point coordinates: pts = dict() pts[1] = ab.Point(0, -35) pts[2] = ab.Point(-50, -35) pts[3] = ab.Point(-50, 35) pts[4] = ab.Point(0, 35) pts[5] = ab.Point(50, 35) pts[6] = ab.Point(50, -35) # Create a segments dictionary referencing point and material ids: sgs = dict() sgs[1] = ab.Segment(1, 2, 1) sgs[2] = ab.Segment(2, 3, 1) sgs[3] = ab.Segment(3, 4, 1) sgs[4] = ab.Segment(4, 1, 1) sgs[5] = ab.Segment(4, 5, 1) sgs[6] = ab.Segment(5, 6, 1) sgs[7] = ab.Segment(6, 1, 1) # Point the dictionaries to the section sc.materials = mts sc.points = pts sc.segments = sgs # Calculate and output section properties
import abdbeam as ab sc = ab.Section() # Create a dictionary to store ply materials shared by laminates ply_mts = dict() ply_mts[1] = ab.PlyMaterial(0.0075, 2.147e7, 1.4e6, 6.6e5, 0.3) ply_mts[2] = ab.PlyMaterial(0.0075, 1.149e7, 1.149e7, 6.6e5, 0.04) # Create the materials dictionary for the laminates and shear connector: mts = dict() mts[1] = ab.Laminate() mts[1].ply_materials[2] = ply_mts[2] mts[1].plies = [[45, 2], [-45, 2]] + [[0, 2]] * 3 mts[1].symmetry = 'S' mts[2] = ab.Laminate() mts[2].ply_materials[2] = ply_mts[2] mts[2].plies = [[45, 2], [-45, 2]] * 2 + [[0, 2]] mts[2].symmetry = 'S' mts[3] = ab.Laminate() mts[3].ply_materials[1] = ply_mts[1] mts[3].ply_materials[2] = ply_mts[2] mts[3].plies = [[45, 2], [-45, 2]] + [[0, 1]] * 3 + [[0, 2]] + [[0, 1]] * 2 mts[3].symmetry = 'SM' mts[4] = ab.ShearConnector(0.075, 2605615) # Create a points dictionary based on Y and Z point coordinates: pts = dict() pts[1] = ab.Point(-2, 0) pts[2] = ab.Point(-1, 0) pts[3] = ab.Point(1, 0) pts[4] = ab.Point(2, 0) pts[5] = ab.Point(-2, 0.075) pts[6] = ab.Point(-1, 0.075)