b) Beam AE designed by 1FKM Sdn Bhd is supported and loaded as shown in Figure Q5b. (1) Draw the free-body diagram of the beam AE. (i) Determine the reaction at the supports A and E. (ii) Draw the shear-force and bending-moment diagrams for the beam AE. (iv) What is the maximum bending moment and at which location does it occur? FBD →²Fx=6²@ ) particle •2ty=0) y M₁ = 0-2a = 0 = ba Rigid bodig hinge 6 kN-m 2 m O B Minch. 2m 2 kN C 4 m ¹7:4kN 1 kN/m MEN D 4 m E NOT ON X isokule object of 야 10 c) Evaluate the shear force and bending moment in terms of a distance x in section CD and their values at a distance 5 m from point A of the beam AE in Figure Q5b.

b) Beam AE designed by 1FKM Sdn Bhd is supported and loaded as shown in Figure Q5b. (1) Draw the free-body diagram of the beam AE. (i) Determine the reaction at the supports A and E. (ii) Draw the shear-force and bending-moment diagrams for the beam AE. (iv) What is the maximum bending moment and at which location does it occur? FBD →²Fx=6²@ ) particle •2ty=0) y M₁ = 0-2a = 0 = ba Rigid bodig hinge 6 kN-m 2 m O B Minch. 2m 2 kN C 4 m ¹7:4kN 1 kN/m MEN D 4 m E NOT ON X isokule object of 야 10 c) Evaluate the shear force and bending moment in terms of a distance x in section CD and their values at a distance 5 m from point A of the beam AE in Figure Q5b.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

The pin-connected structure consists of a rigid beam ABCD and two supporting bars. Bar (1) is an aluminum alloy [E = 77 GPa) with a cross-sectional area of A₁ = 790 mm². Bar (2) is a bronze alloy [E = 98 GPa] with a cross-sectional area of A2 = 550 mm². Assume L₁=2.6 m, L₂=3.3 m, a=0.8 m, b=1.4 m, and c=1.2 m. All bars are unstressed before the load P is applied; however, there is a 3-mm clearance in the pin connection at A. If a load of P = 38 kN is applied at B, determine: (a) the normal stresses 01, 02, in both bars (1) and (2). (b) the normal strains &1, 2, in bars (1) and (2). (c) determine the downward deflection VA of point A on the rigid bar. (1) Answers: (a) σ₁ = (b) ₁ = (c) VA = i i L₁ B b (2) C MPa, 0₁ = L2 με, €2 = i mm. i D MPa. με.
Determine the support reactions. ** need asap pls. Thanks.
B found that the member AC is fabricated A frame shown in the above figure, it was When fabricating the pin-jointed plane members after assembly. All members hay 60° 30° 30° 30° A 30° D a Jrame shown in the above figure, u was Jound that the member AC is fabricated A too long. Determine the forces in the members after assembly. All members hav same axial stiffness (AE)
Solve the forces in each member in terms of force P.
The members of the truss shown below have a cross-sectional area of 10,000 mm2. Determine the stresses in members AB and AE in MPa. Indicate if the stresses are in compression or tension. -3 m- -3 m- C E 40 kN 80 kN A 6m- 3m-
Determine the shear lag factor of the connection shown in the figure.
A prismatic beam (as shown below) has plastic moment capacity of Mp, then the collapse load Pof the beam is P P/2 L/2 – - L/2 + L/3
The pin-connected structure consists of a rigid beam ABCD and two supporting bars. Bar (1) is an aluminum alloy [E = 61 GPa] with a cross-sectional area of A₁ = 810 mm². Bar (2) is a bronze alloy [E = 103 GPa] with a cross-sectional area of A2 = 470 mm². Assume L₁=2.4 m, L₂=3.1 m, a=0.7 m, b=1.9 m, and c= 1.1 m. All bars are unstressed before the load P is applied; however, there is a 5.8-mm clearance in the pin connection at A. If a load of P = 44 kN is applied at B, determine: (a) the normal stresses 0₁, 0₂, in both bars (1) and (2). (b) the normal strains &1, 82, in bars (1) and (2). (c) determine the downward deflection VA of point A on the rigid bar. A Answers: (a) 0₁ = (STVA = a i i B 156.10 0.00256 b C MPa, 0₁ = με, €2 = mm L2 i i D 20.75 0.0002014 MPa. με.
Determine the stresses in each bar and the bond reactions.
A2
The pin-connected structure consists of a rigid beam ABCD and two supporting bars. Bar (1) is an aluminum alloy [E = 74 GPa] with a cross-sectional area of A₁ = 820 mm². Bar (2) is a bronze alloy [E = 117 GPa] with a cross-sectional area of A₂ = 420 mm². Assume L₁=1.9 m, L₂=2.5 m, a=0.7 m, b=1.9 m, and c=1.3 m. All bars are unstressed before the load P is applied; however, there is a 1.4-mm clearance in the pin connection at A. If a load of P = 34 KN is applied at B, determine: (a) the normal stresses 0₁, 02, in both bars (1) and (2). (b) the normal strains &1, 2, in bars (1) and (2). (c) determine the downward deflection VA of point A on the rigid bar. (1) A Answers: (a) σ₁ = (b) ₁: (c) VA = = tel i L₁ B b L2 mm. C MPa, σ₁ = με, εξ = i i D MPa. με.
The pin-connected structure consists of a rigid beam ABCD and two supporting bars. Bar (1) is an aluminum alloy [E = 79 GPa] with a cross-sectional area of A₁ = 700 mm². Bar (2) is a bronze alloy [E = 106 GPa] with a cross-sectional area of A₂ = 480 mm². Assume L₁=1.8 m, L₂=2.1 m, a=0.5 m, b=1.6 m, and c=0.8 m. All bars are unstressed before the load P is applied; however, there is a 3.4-mm clearance in the pin connection at A. If a load of P = 53 kN is applied at B, determine: (a) the normal stresses 01, 02, in both bars (1) and (2). (b) the normal strains 1, 2, in bars (1) and (2). (c) determine the downward deflection VA of point A on the rigid bar. (1) A Answers: (a) σ₁ = (b) 1 (c) VA = i a L₁ B b (2) L2 MPa, 0₁ = με, €2 = mm. i i D MPa. με.