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7/19/2024 <br /> Sheet A.10 <br />Prepared by PB <br />Checked by AY <br />Target T0286- Santa Ana – Final Report PPE-05184.03 <br />Span 2 loads <br /> Dead point load 4258 lb at 78.00 in <br /> Dead point load 10765 lb at 144.00 in <br />Load combinations <br />Load combination 1 Support A Dead ´ 1.40 <br /> Live ´ 0.00 <br /> Span 1 Dead ´ 1.40 <br /> Live ´ 0.00 <br /> Support B Dead ´ 1.40 <br /> Live ´ 0.00 <br /> Span 2 Dead ´ 1.20 <br /> Live ´ 1.60 <br /> Support C Dead ´ 1.20 <br /> Live ´ 1.60 <br />Analysis results <br />Maximum moment;Mmax = 348135 lb_ft; Mmin = -193943 lb_ft <br />Design moment; M = max(abs(Mmax),abs(Mmin)) = 348135 lb_ft <br />Maximum shear; Fmax = 21303 lb; Fmin = -32406 lb <br />Design shear; F = max(abs(Fmax),abs(Fmin)) = 32406 lb <br />Total load on member; Wtot = 72689 lb <br />Reaction at support A; RA_max = 21303 lb; RA_min = 21303 lb <br />Unfactored dead load reaction at support A; RA_Dead = 14861 lb <br />Reaction at support B; RB_max = 51386 lb; RB_min = 51386 lb <br />Unfactored dead load reaction at support B; RB_Dead = 39319 lb <br />Reaction at support C; RC_max = 0 lb; RC_min = 0 lb <br />Unfactored dead load reaction at support C; RC_Dead = 0 lb <br />Glulam section details <br />Net finished breadth of sections; b = 7 in <br />Net finished depth of sections; d = 38.875 in <br />Number of sections in member; N = 1 <br />Overall breadth of member; bb = N ´ b = 7 in <br />Alignment of laminations; Horizontal <br />Stress class; 24F-V8 DF/DF <br />Tension parallel to grain; Ft = 1100 lb/in2 <br />Compression parallel to grain; Fc = 1650 lb/in2 <br />Bending about X-X axis properties (loaded perpendicular to wide faces of laminations): <br />Positive bending; Fbx_pos = 2400 lb/in2 <br />Negative bending; Fbx_neg = 2400 lb/in2 <br />Compression perpendicular to grain; Fc_perp = 650 lb/in2 <br />Shear parallel to grain; Fv = 265 lb/in2 <br />Modulus of elasticity; E = 1800000 lb/in2 <br />Modulus of elasticity, stability calculations; Emin = 950000 lb/in2 <br />Mean shear modulus; Gdef = E / 16 = 112500 lb/in2 <br />Bending about Y-Y axis properties (loaded parallel to wide faces of laminations): <br />Bending; Fby = 1550 lb/in2 <br />1330 E Seventeenth <br />St4/10/2025