

1. For the doubly section shown in Figure, determine the cracking moments iff-25 MPa. 100 600...
Figure 1 shows the cross section of a lipped channel. The cross section carries a shear force of 250 kN acting at 45° below the major principal axis (as shown) and through the shear centre. Determine the Ans: 134.1 MPa) maximum shear stress. (Use line of mid-thickness properties) t 45 34 S.C 250 N たA 100 Figure
7. Evaluate M, for the section shown in Figure 3.9(2). Assume f = 20 MPa. 200 t 100 @ 2 N24 500 4 N24 1001 Figure 3.9(2) Cross-sectional details of the example beam section Note: all dimensions are in mm.
1) The allowable bending strength in A-A cross section is Oallow= 150 MPa. Determine the maximum load P where it applied to the bar from point E (40 points). Figure 1 D 600 mm a 300 mm 20 mm В. 50 mm 25 mm 25 mm 25 mm A-A cross section
WORKING with Plates-PLATE#3 3. For the cross-section shown in Figure 3, (a) determine the bending moment that the reinforced concrete section can cary If As 1200 mm2. (b) determine the maximum area of steel that can be used In this section and (c) determine the maximum moment that can be resisted by the section. Use Fc 25 MPa, fy 400 Mpa 250 HGURE uaugo9-p
5. Determine the mid-span short-term deflection of a simply supported beam with the section shown in Figure Q5. Design data: Concrete strength: fcu 30 MPa. Area of tensile steel reinforcement: As 1500 mm Area of compressive steel reinforcement: A,-1500 mm2 Instantaneous static modulus of elasticity of concrete = 25GPa. Span -8.0 m Loading: Dead load 5.0 kN/m (uniformly distributed load); Live load 5.0 kN/m (uniformly distributed load) (Hint: the height of neutral axis of the mid-span section under the service...
A beam with cross-section as shown in Figure 2(a) is made of an
elasto-plastic material. The stressstrain relationship of the
material is as shown in Figure 2(b): (a) A bending moment is
applied to this section and increased until the entire top flange
yielded. Calculate the magnitude of the moment at this stage of
loading. (b) Determine the yield moment of the beam (c) Determine
the ultimate moment capacity of the beam (d) Determine the shape
factor of the beam...
Q5 Consider an extruded aluminium machine part that has the cross-section shown in the accompanying figure. Determine the maximum moment M that can be applied to the member if the allowable bending stresses in tension and compression are 200 MPa and 100 MPa respectively 100 mm 25 mm NA 50 mm 25 mm 50 mm 25 mm
Figure 1 shows the cross section of a lipped channel. The cross section carries a shear force of 250 kN acting at 45° below the major principal axis (as shown) and through the shear centre. Determine the (Ans: 134.1 MPa) maximum shear stress. (Use line of mid-thickness properties) た45 S.c 4250 N たA 100 Figure 1
Figure 1 shows the cross section of a lipped channel. The cross section carries a shear force of 250 kN acting at 45° below...
3- Determine the maximum shear stress in the beam section shown in the figure. Determine also the rate of twist of the beam section if the shear modulus G is 25 GPa. 100 mm T-25 N.m 3 mm 3 mm 50 mm 80 mm 2 mm
3- Determine the maximum shear stress in the beam section shown in the figure. Determine also the rate of twist of the beam section if the shear modulus G is 25 GPa. 100 mm...
For the section and material properties shown in Figure 1, calculate the moment and corresponding curvature given a compressive strain at the top fibre of 0.0036 and a neutral axis depth of 48 mm. [6 marks] Perform only one iteration regardless of convergence. 0.0036 E 25 mm 48 mm 220 mm 325 mm 350 mm 675 mm You 250 mm E = 200 GPS Es - 7500 MPa f = 500 MPa f = 40 MPa E = 0.0018 &...