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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 Find the lightest angled beam. [pause] In this problem, an L beam is --- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 subjected to a tensile force, P. The beam is fastened to a plate with 3 bolts --- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 in a line, of a given bolt diameter. The type of steel and --- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 factored load are provided, as well as the length of the beam, L, and --- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 reduction coefficient, U. [pause] If we look ahead ---- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin plate L beam neglect block shear failure A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 to the possible solutions, and organize them in a table, ---- P
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # we’ll select the lightest beam which satisfies the strength requirement, --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # and slenderness requirement. We’ll first check each beam for the --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
γ * Q = 84,000 [lb] steel A572 grade 50 L = 12 [ft] U = 0.85 L ≤ 240 dbolt = 7/8 [in] rmin Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # slenderness requirement, which states the length of the beam, --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] rmin Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # divided by the minimum radius of gyration, shall not exceed 240. L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] rmin L rmin ≥ 240 Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # If we solve for r min, and plug in the length of the beam, L, --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ 240 Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # in inches, the minimum permissible radius of gyration equals, --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ rmin ≥ 0.60 [in] 240 Beam Strength Slender Weight L 4 x 4 x 5/16 ? ? # 0.60 inches. [pause] Therefore, if any of the L beams have a radius of gyrations smaller than --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ rmin ≥ 0.60 [in] slenderness 240 requirement r [in] Beam Strength Weight L 4 x 4 x 5/16 ? ? # 0.60 inches, they are too slender, and hence disqualified from the selection. After looking up --- L3.5x3.5x3/8 ? ? # L 3 x 3 x 7/16 ? ? # L 4 x 3 x 3/8 ? ? #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ rmin ≥ 0.60 [in] slenderness 240 requirement r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # the minimum radius of gyration values, for each beam, we notice all 4 beams --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ rmin ≥ 0.60 [in] slenderness 240 requirement r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # exceed the minimum requirement, and none are disqualified, based on ---- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
≤ 240 L = 12 [ft] 12 rmin * ft L rmin ≥ rmin ≥ 0.60 [in] slenderness 240 requirement r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # the slederness requriement. [pause] Next we’ll check each beam for the ---- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
≤ 240 rmin L rmin ≥ 240 rmin ≥ 0.60 [in] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # strength requirement. Since the problem states to neglect --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
≤ neglect block 240 rmin shear failure L rmin ≥ 240 rmin ≥ 0.60 [in] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # block shear failure, we know the strength requirement will be based on either --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: neglect block 1. yield shear failure 2. fracture rmin ≥ 0.60 [in] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # a yield-type failure, or fracture-type failure. [pause] In each case, the factored load, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # gamma Q, shall not exceed the design strength, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture factored design load strength r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # R phi. From the problem statement we know the --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture factored design load strength γ * Q = 84,000 [lb] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # factored load equals, 84,000 pounds. Next, we’ll compute the design strength --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture factored design load strength γ * Q = 84,000 [lb] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # for each failure mode, determine which failure mode governs, ---- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture factored design load strength γ * Q = 84,000 [lb] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # and then compare whether or not each of the 4 L beams satisfy --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
γ * Q ≤ φ * R failure mode: 1. yield 2. fracture factored design load strength γ * Q = 84,000 [lb] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # the strength requirement. We’ll first look at a yield-type failure, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 84,000 [lb] ≤ φyield * Ryield 1. yield 2. fracture r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # where the strength reduction factor, phi yield, equals, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 84,000 [lb] ≤ φyield * Ryield 1. yield 0.9 2. fracture r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # 0.9, and the resistance term, R yield, equals, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 84,000 [lb] ≤ φyield * Ryield 1. yield 0.9 2. fracture fy * Agross r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # the yield stress times the gross area of the beam. The problem states the steel is --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 84,000 [lb] ≤ φyield * Ryield 1. yield 0.9 2. fracture fy * Agross A572 grade 50 r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # type A572 grade 50, which has a yield stress of --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 84,000 [lb] ≤ φyield * Ryield 1. yield 0.9 2. fracture fy * Agross A572 grade 50 fy=50,000 [lb/in2] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # 50,000 pounds per square inch. Next, if we isolate the gross area term, the gross area of the beam --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
Agross≥ 1.86 [in2] failure mode: 1. yield 84,000 [lb] ≤ φyield * Ryield 2. fracture 0.9 fy * Agross A572 grade 50 fy=50,000 [lb/in2] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # shall be at least 1.86 inches squared. [pause] Now we’ll examine --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fy=50,000 [lb/in2] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # a fracture-type failure. Where the strength reduction factor, phi fracture, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fy=50,000 [lb/in2] r [in] Beam Strength Weight L 4 x 4 x 5/16 ? 1.24 # equals, 0.75, and the resistance term, R fracture, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu * Ae Beam Strength L 4 x 4 x 5/16 ? equals the ultimate stress of the steel, f u, times the effective area of the steel, --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu * Ae Beam Strength ultimate L 4 x 4 x 5/16 ? stress A e. [pause] Given the type of steel, we know the ultimate stress equals, --- L3.5x3.5x3/8 ? effective L 3 x 3 x 7/16 ? area L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? 65,000 pounds per square inch. And the effective area, A e, equals, --- ultimate L3.5x3.5x3/8 ? stress L 3 x 3 x 7/16 ? effective L 4 x 3 x 3/8 ? area
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? the net area, A net, times, U, the reduction coefficient. The problem states --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? effective L 4 x 3 x 3/8 ? area
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? the reduction coefficient, equals, Therefore, if we solve for --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? the net area, we find that the net area of the beam shall be at least, --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
failure mode: 0.75 Agross≥ 1.86 [in2] 1. yield 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? 2.03 inches squared. [pause] Since the net area will never be greater than --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ? Anet≥ 2.03 [in2]
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Find: Lightest Angled Beam
Anet ≤ Agross failure mode: Agross≥ 1.86 [in2] 1. yield 0.75 2. fracture 84,000 [lb] ≤φfracture * Rfracture A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? the gross area, a fracture-type failure strength requriement is more conservative, --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ? Anet≥ 2.03 [in2]
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Find: Lightest Angled Beam
Anet ≤ Agross failure mode: Agross≥ 1.86 [in2] 1. yield 2. fracture Anet≥ 2.03 [in2] A572 grade 50 fu=65,000 [lb/in2] Beam Strength fu * Ae L 4 x 4 x 5/16 ? and will serve as the governing equation for the strength requirement of the L beam. Therefore, --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ? Anet≥ 2.03 [in2]
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Find: Lightest Angled Beam
Anet ≤ Agross failure mode: Agross≥ 1.86 [in2] 1. yield 2. fracture Anet≥ 2.03 [in2] A572 grade 50 fu=65,000 [lb/in2] Beam Anet [in2] fu * Ae L 4 x 4 x 5/16 ? we’ll compute the net area of each L beam, and compare it’s values to the --- Ae=Anet * U L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? U=0.85 L 4 x 3 x 3/8 ? Anet≥ 2.03 [in2]
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Find: Lightest Angled Beam
Anet ≤ Agross failure mode: Agross≥ 1.86 [in2] 1. yield 2. fracture Anet≥ 2.03 [in2] A572 grade 50 Beam Anet [in2] L 4 x 4 x 5/16 ? minimum required net area. As an example, we’ll compute --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet ≤ Agross failure mode: Agross≥ 1.86 [in2] 1. yield 2. fracture Anet≥ 2.03 [in2] A572 grade 50 Beam Anet [in2] L 4 x 4 x 5/16 ? the net area for beam L 4 by 4 by 5/16. Which equals, --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t Anet≥ 2.03 [in2] Beam Anet [in2] L 4 x 4 x 5/16 ? the gross area of the beam, minus the number of holes along the fracture path, times --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t gross thickness bolt area diameter Anet≥ 2.03 [in2] Beam Anet [in2] L 4 x 4 x 5/16 ? the quantity, the diameter of the bolt plus 1/8 inch, times the thickness of the beam. L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t gross thickness bolt area diameter Anet≥ 2.03 [in2] Beam Anet [in2] L 4 x 4 x 5/16 ? For a 4 by 4 by 5/16 L beam, the gross area equals, --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 5/16 [in] bolt diameter Beam Anet [in2] Anet≥ 2.03 [in2] L 4 x 4 x 5/16 ? 2.40 inches squared, and the thickness equals, 5/16 inches. [pause] From the diagram, --- L3.5x3.5x3/8 ? L 3 x 3 x 7/16 ? L 4 x 3 x 3/8 ?
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 5/16 [in] bolt diameter Anet≥ 2.03 [in2] we notice the fracture path would only pass through ---- P
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 5/16 [in] bolt diameter fracture path Anet≥ 2.03 [in2] 1 bolt hole, therefore the number of holes in the equation, equals, --- P
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 5/16 [in] bolt 1 diameter fracture path Anet≥ 2.03 [in2] 1. [pause] The problem provides the bolt diamter, as, --- P
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 7/8 [in] 5/16 [in] 1 fracture path Anet≥ 2.03 [in2] 7/8 of an inch, and the 1/8 inch term accounts for ---- P
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 7/8 [in] 5/16 [in] 1 hole diameter & fracture path damaged thickness the diameter of the hole and the damaged thickness around the hole. P
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 7/8 [in] 5/16 [in] 1 Beam Anet [in2] r [in] Weight L 4 x 4 x 5/16 ? 1.24 # After plugging in our values, the net area for a 4 by 4 by 5/16 L beam, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- # holes * ( dbolt + 1/8 [in] ) * t 2.40 [in2] 7/8 [in] 5/16 [in] 1 Anet,4x4x5/16 = 2.09[in2] Beam Anet [in2] r [in] Weight L 4 x 4 x 5/16 2.09 1.24 # equals, 2.09 inches squared. [pause] This calculation is repeated for the other 3 beam sizes, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t Agross,3.5x3.5x3/8 t3.5x3.5x3/8 Agross,3x3x7/16 t3x3x7/16 Agross,4x3x3/8 t4x3x3/8 Anet [in2] r [in] Beam Weight L 4 x 4 x 5/16 2.09 1.24 # using the gross area and thickness unique to each beam. Once all the areas are computed, --- L3.5x3.5x3/8 ? 1.07 # L 3 x 3 x 7/16 ? 0.905 # L 4 x 3 x 3/8 ? 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t Agross,3.5x3.5x3/8 t3.5x3.5x3/8 Agross,3x3x7/16 t3x3x7/16 Agross,4x3x3/8 t4x3x3/8 Anet [in2] r [in] Beam Weight L 4 x 4 x 5/16 2.09 1.24 # we’ll check if each beam meets the minimum net area --- L3.5x3.5x3/8 2.11 1.07 # L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t Anet≥ 2.03 [in2] Beam Anet [in2] r [in] Weight L 4 x 4 x 5/16 2.09 1.24 # which is not met by L 3 by 3 by 7/16 beam , so we can remove this beam from --- L3.5x3.5x3/8 2.11 1.07 # L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t Anet≥ 2.03 [in2] Beam Anet [in2] r [in] Weight L 4 x 4 x 5/16 2.09 1.24 # out list of potential beams. For the 3 beams which pass the strength requirement ---- L3.5x3.5x3/8 2.11 1.07 # L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t strength slenderness requirement requirement Anet [in2] r [in] Beam Weight L 4 x 4 x 5/16 2.09 1.24 # and slenderness requirement, we’ll look up their linear weights, to find, ---- L3.5x3.5x3/8 2.11 1.07 # L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 #
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Find: Lightest Angled Beam
Anet = Agross- 1* ( 7/8 [in] + 1/8 [in] ) * t strength slenderness requirement requirement [lb/ft] r [in] Beam Anet [in2] Weight L 4 x 4 x 5/16 2.09 1.24 8.20 beam L 4 by 4 by 5/16 is the lightest beam. [pause] L3.5x3.5x3/8 2.11 1.07 8.50 L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 8.50
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Find: Lightest Angled Beam
A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 slenderness requirement [lb/ft] r [in] Beam Anet [in2] Weight L 4 x 4 x 5/16 2.09 1.24 8.20 When reviewing the possible solutions, --- L3.5x3.5x3/8 2.11 1.07 8.50 L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 8.50
65
Find: Lightest Angled Beam
A) L 4 x 4 x 5/16 B) L 3.5x3.5x3/8 C) L 3 x 3 x 7/16 D) L 4 x 3 x 3/8 answerA slenderness requirement [lb/ft] r [in] Beam Anet [in2] Weight L 4 x 4 x 5/16 2.09 1.24 8.20 the correct answer is A. L3.5x3.5x3/8 2.11 1.07 8.50 L 3 x 3 x 7/16 1.99 0.905 # L 4 x 3 x 3/8 2.11 0.879 8.50
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