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Solve the two problems below using the finite element method with Euler-Bernoulli beam element. 2...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P= 10 KN W = 10 kN/m 200 mm 5 m 5 m...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN W = 10 kN/m 200 mm 5 m 5...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN w = 10 kN/m 200 mm 5 m 5...
A rectangular cross section at a location along a beam in bending is
(a). A rectangular cross section at a location along a beam in bending is acted upon by a bending moment and a shear force. The cross section is \(120 \mathrm{~mm}\) wide, \(300 \mathrm{~mm}\) deep and is orientated such that it is in bending about its major axis of bending. The magnitudes of the bending moment and shear force are \(315 \mathrm{kNm}\) and \(240 \mathrm{kN}\) respectively. Determine the maximum bending and shear stresses on the cross section. Plot the bending and...
39. Solve the following frame structure using a commercial finite element analysis program. The f...
39. Solve the following frame structure using a commercial finite element analysis program. The frame structure is under a uniformly distributed load of q 1000 N/m and has a circular cross section with radius r 0.1 m. For material property, Young's modulus E 207 GPa Plot the deformed geometry with an appropriate magnifica- tion factor, and draw a bending moment and shear force diagrams. 2 m 2 m
39. Solve the following frame structure using a commercial finite element analysis...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform t...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to determine the deflection and stress of bottom surface. (2.) Using elementary beam theory to determine the deflection and stress of bottom surface
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to...
The simply supported beam of length L is subjected to uniformly distributed load of w and...
The simply supported beam of length L is subjected to uniformly distributed load of w and a vertical point load P at its middle, as shown in Figure Q3. Both young's modulus and second moment of area of this structure are given as E and I. Please provide your answers in terms of letters w, P,L,1, E. Self-weight of the beam is neglected. P W L/2 L/2 Figure Q3 (a) Determine the reactions, bending moment equation along the beam and...
A beam with length L-2 m and rectangular cross-section of width b-75 mm and height h...
A beam with length L-2 m and rectangular cross-section of width b-75 mm and height h 150 mm has a uniformly distributed load of intensity q 2.5 kN/m (see figure below). What is the maximum deflection δmax in millimeters? The material is aluminum with modulus of elasticity E 70 GPa. T77
Strength of Materials IV 9.2-5 The defiuction curve for a cantilever beam AB (see fgure) is given b 120LEI Describe the load acting on the beam. 2 .3-6 Calculate the maximum deflectio...
Strength of Materials IV
9.2-5 The defiuction curve for a cantilever beam AB (see fgure) is given b 120LEI Describe the load acting on the beam. 2 .3-6 Calculate the maximum deflection dma of a uniformly loaded simple beam if the span length L 5 2.0 m, the intensity of the uniform load g 5 2.0 kN/m, and the maximum bending stress s 5 60 MPa. rn X The cross section of the beam is square, and the material is...
x Incorrect Two beams support a uniformly distributed load of w = 28 kN/m, as shown....
x Incorrect Two beams support a uniformly distributed load of w = 28 kN/m, as shown. Beam (1) is supported by a fixed support at A and by a simply supported beam (2) at D. In the unloaded condition, beam (1) touches, but exerts no force on, beam (2). Beam (1) has a depth of 300 mm, a moment of inertia of 11 = 125 x 106 mm, a length of L = 3.4 m, and an elastic modulus of...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P= 10 KN W = 10 kN/m 200 mm 5 m 5 m...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN W = 10 kN/m 200 mm 5 m 5...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN w = 10 kN/m 200 mm 5 m 5...
39. Solve the following frame structure using a commercial finite element analysis program. The frame structure is under a uniformly distributed load of q 1000 N/m and has a circular cross section with radius r 0.1 m. For material property, Young's modulus E 207 GPa Plot the deformed geometry with an appropriate magnifica- tion factor, and draw a bending moment and shear force diagrams. 2 m 2 m
39. Solve the following frame structure using a commercial finite element analysis...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to determine the deflection and stress of bottom surface. (2.) Using elementary beam theory to determine the deflection and stress of bottom surface
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to...
The simply supported beam of length L is subjected to uniformly distributed load of w and a vertical point load P at its middle, as shown in Figure Q3. Both young's modulus and second moment of area of this structure are given as E and I. Please provide your answers in terms of letters w, P,L,1, E. Self-weight of the beam is neglected. P W L/2 L/2 Figure Q3 (a) Determine the reactions, bending moment equation along the beam and...
A beam with length L-2 m and rectangular cross-section of width b-75 mm and height h 150 mm has a uniformly distributed load of intensity q 2.5 kN/m (see figure below). What is the maximum deflection δmax in millimeters? The material is aluminum with modulus of elasticity E 70 GPa. T77
Strength of Materials IV
9.2-5 The defiuction curve for a cantilever beam AB (see fgure) is given b 120LEI Describe the load acting on the beam. 2 .3-6 Calculate the maximum deflection dma of a uniformly loaded simple beam if the span length L 5 2.0 m, the intensity of the uniform load g 5 2.0 kN/m, and the maximum bending stress s 5 60 MPa. rn X The cross section of the beam is square, and the material is...
x Incorrect Two beams support a uniformly distributed load of w = 28 kN/m, as shown. Beam (1) is supported by a fixed support at A and by a simply supported beam (2) at D. In the unloaded condition, beam (1) touches, but exerts no force on, beam (2). Beam (1) has a depth of 300 mm, a moment of inertia of 11 = 125 x 106 mm, a length of L = 3.4 m, and an elastic modulus of...
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