A W18x55 has been selected for the beam as shown. Determine the value of w that the beam can carry in addition to its weight using A-50 steel assuming full lateral support. 7300 SNAS W 9000
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- For the box beam shown in Fig. if the modulus of elasticity E = 200 GPa, the flexural stresses at support for point (a) is ..................... MPa * 120mm 16.2kN 16.2KkN —{ 10.2KN/m £ fj//’/ £ W @ Q| im 3m im = 30 mm thickness of walls cross section Your answerDetermine the design strength of a T- Beam given the following data: bf = 700 mm bw = 300 mm hf = 100 mm d = 500 mm %3D fe' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.determine the member stresses of the truss shown. indicate if the stress in the member is in tension or compression. present complete and neat solutions. p1-30kN W-25kN/m P2=51kN AH Av Im P₂ Im P₂ Im P₂ Im Av W 1.6m
- NO. 1. What is the maximum bending stress in the uniformly loaded cantilever beam as shown if the depth of the beam is h = 250mm, the maximum deflection is 8max = 5mm, the span is L = 3m, and the modulus of elasticity is E = 70 GPa. Use any method. Wo L max A B 4-TDetermine the design strength of a T-Beam with the following data: b+= 700 mm bw = 300 mm hy = 100 mm d = 500 mm f₂ = 21 MPa fy = 414 MPa A: 5-20 mm dia.Problem: A W14 x 74 beam-column member in a braced frame must support the service loads shown in the figure. The member is A992 steel and bending is about the strong axis. The member is laterally braced at its ends only. Do not consider moment amplification. Determine whether the given member satisfies the appropriate AISC interaction equation. Use (a) ASD, and (b) LRFD PD = 534 kN PL = 1068 kN MD = 20 kN-m ML = 54 kN - m W14 x 74 4.9 m Kx = 0.85; Ky = 1.0 Mp = 24.4 kN-m ML = 65 kN-m Pp = 534 kN PL = 1068 kN
- Determine the design strength of a T- Beam with the following data: bf = 700 mm bw = 300 mm h = 100 mm d = 500 mm fe = 21 MPa fy = 414 MPa Ag: 5- 20 mm dia.A cast iron beam is of I-section as shown in figure below. The beam is simply supported on a Span of 5 meters. If tensil Stress is not execed 20 N/mm², find the safe uniformly load which the beam can carry. find also the maximum Compressive Stress. 25mm k120mm. 300mm T 50mm ↓ B 25mm ← 240- 키Q4 For the simply supported beam shown in Figure below, design the cross section against the maximum bending moment using Working Stress Method. The width of beam is 300 mm. Use 025 mm, fe 10 Mpa, f, = 140 Mpa and n-10. %3D P-40 kN WD L) 14.32 kN/m (Including self-weight) L-8m
- An aluminum alloy (E=73GPA) bar is loaded and supported as shown. The diameters of the top and bottom section of the bar are 25mm and 15mm, respectively. Determine the deflection of section b-b. Neglect the weight of the bar 1.2 m 1.5 m 20 kN a 1.5m 15KN 20 kNFrom the given figure below, determine the minimum height of the beam if the flexural stress is not to exceed 50kPa. Assume width of beam is 200mm (JN 10 N/m 0- T 3M RA=42N 42N B IM TEMA 12N 75NM 81NM, Im RD=3N EL -3N 0° 78 Nm 3NM V-DIAG M-DIAGThe tee section shown below is to carry a bending moment of 8440 N·m. It is to be made of steel plates welded together. If the load on the beam is a static load, would SAE 1020 hot-rolled steel be satisfactory for the plates? -175 mm 25 mm 200 mm 25 mm