Determine the design strength of a T- Beam given the following data: bf = 700 mm bw = 300 mm hf = 100 mm d = 500 mm fc' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.
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Determine the design strength of a T- Beam given the following data:
bf = 700 mm
bw = 300 mm
hf = 100 mm
d = 500 mm
fc' = 21 MPa
fy = 414 MPa
As: 5- 20 mm dia.
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- Determine 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 design strength of a T- Beam given the following data: b = 700 mm by = 300 mm hf = 100 mm d = 500 mm fe' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.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.
- Fill in the blanks: For the given properties of the beam below, determine the safest wy that the beam will carry. bf = 850mm bw = 400mm tf = 100mm d = 400mm d' = 100mm fc' = 32MPA fy = 400MPA As = 8-32mm bars %3D The answer is kN/m Pu = 20 KN bf 3Pu O-50 Pu 1m As A 13 + bw + CS Scanned with CamScannerDetermine the Design Flexural Strength of W460x52 A992 Steel with the following cases: CIVIL ENGINEERING STEEL DESIGN With Continuous lateral bracing Unbraced length = 4m, Cb = 1.0 Unbraced length= 12m, Cb = 1.0 a.) b.) c.) Fy = 345 MPa Properties: d = 450mm tf = 10.8 mm 1x 212x10mm* Cw 306x10 mm" Sx** 944 x10¹mm¹ bf 142mm MY Ag - 6650mm2 Zx 1090x10'mm' Ho439mm ry = 31mm tw* 7.62mm J-211x10¹mm* ly = 6.37x10 mm rls - 38.4mmA simply supported beam shown below is HEA 400 of 5355 steel. It is laterally supported at points with an "X" The material properties and the section properties are given below. Use ASD load combination DL+LL and determine whether the beam has adequate flexural strength. Material: $355 Fy= 355 MPal Fu= 510 MPa E= 200000 MPa Section properties: A: 15900 mm² d: 390 mm h: 298 mm b: 300mm tr: 19 mm W 2311x10³ mm³ Iy: 8564x10*mm* A 4m t: 11 mm. İy: 73.4 mm W: 2563x10³ mm³ J: 189x104 mm DL: 150 KN LL: 100 KN 17 B 4m Cw: 2942x10⁹ mm C E: 200000 MPa
- 1) Calculate maximum deflection of the beams. 2) Check the suitability of the section assuming the code limitation of L/240. 3) If maximum deflection doesn't meet the code requirement, propose your solution. 1 UKB 457 x 152x82 Steel: Section properties: I=366,000,000 mm². E=2*(10)³ N/mm² A 4m 200kN 2m Please use this formula below, thank you фи k-c: W *a* ·b- a≤ b, c=√√b(L+a) K-c→B Wac³ 3LEI (at position c)3) For the concrete beams shown, draw the approximate deflection shape and draw the locations of the reinforcing bars (top or bottom) for the following beams Fixed Pin & b & b сб $ के के bbbbbb کن के Fin roller fixed b dd freeFor the composite area shown: 1. Locate the centroid in the x and y direction? 2. Find the moment of inertia about the x axis? 180mm 180mm 80mm 80mm 150mm 60mm B I U S X2 OE Shot by Hisense H12 1.
- Permissible As in sechion to ensure tensile Compute the design strength of beam shown it 420 MPa , fc = 30 MPa . check the maximum %3D Permissible As in sechion to ensure tensile failure. 4¢25 stimpp10 q00 8432 300 mm25mm 500 mm Data Given Let steel tube denoted as 1 and brass rod denoted as 2 d10= 40mm E1 = 200GPA dii = 30mm E2 80 GPa d2 25mm A composite bar is made up of a brass rod of 25m diameter enclosed in a steel tube, being co-axial of 40mm external diameters and 30mm internal diameter as shown in the figure. They are securely fixed at each end. If the stress in brass and steel are not to exceed 70MPA and 120 MPa respectively find the change in length, if the composite bar is 500mm long. Take E for steel Tube as 200 GPa and brass rod as 80 GPa respectively. (if P is a safe load that can be carried by the materials) *6. Give the properties table below. A992 Steel 7178 T76 Aluminum Yield Strength 50 ksi 73 ksi Ultimate strength 75 ksi 85 ksi Modulus of Elasticity 29,000 ksi 10,500 ksi Assume you are designing a rectangular member with a specific allowed height. For a design where deflection criterion controls which material would require a larger cross section? For a design where tension stress controls, which material requires the larger cross section?