Q1 For the composite beamshown in fig. 1. Draw bendingstress distribution .if E₁= 20 000MPa., E22000 MPa.E120 000 MPa20 MM-MATERIAL 1E22000 MPa10 kNA-4 MB50 MMMATERIAL 2100 MM-2 M-200 MM-

Here's how to solve it:Information:Inner wall:Material: BrickThickness (L1): 15 cm (0.15 m)Thermal…

Answered: Q1 For the composite beam shown in fig.…

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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The composite shaft shown in the figure consists of a bronze sleeve (1) securely bonded to an inner steel core (2). The bronze sleeve has an outside diameter of 25 mm, an inside diameter of 20 mm, and a shear modulus of G1 = 41 GPa. The solid steel core has a diameter of 20 mm and a shear modulus of G2 = 82 GPa. Assume L = 350 mm. The composite shaft is subjected to a torque of T = 910 N-m. Determine (a) the maximum shear stresses in the bronze sleeve and the steel core. (b) the rotation angle of end B relative to end A. T (1) (2) В
Problem 2 For the beam shown in the figure A) Draw the shear-force and bending-moment diagrams for the beam shown in the figure. B) For the composite section, aluminium [E = 70 GPa] bonded to a steel [E = 210 GPa], located at the maximum bending moment, determine: (1) the maximum bending stresses in the aluminium and steel bars. (2) the stress in the two materials at the joint where they are bonded together. K4N/M 2m B 10kN/mm 4m 2m D Steel Aluminum 42mm 20 mm 13 mm
A small aluminum alloy [E = 79 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 155 mm. The cross- sectional dimensions of the tee shape are b = 16 mm, d = 24 mm, and t = 8 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 410 uɛ is measured from a strain gage located at c = 9 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? 3P Strain gage - d D E H b Answer: P= i N
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Problem 2 For the beam shown in the figure A) Draw the shear-force and bending-moment diagrams for the beam shown in the figure. B) For the composite section, aluminium [E = 70 GPa] bonded to a steel [E = 210 GPa], located at the maximum bending moment, determine: (1) the maximum bending stresses in the aluminium and steel bars. (2) the stress in the two materials at the joint where they are bonded together. K4N/M 2m B 10kN/mm 4m 2m D Steel Aluminum 42mm 20 mm 13 mm
The stress-strain diagram for polyester resin is shown in the figure. Both strut AB and column CD, madefrom this material, support the rigid beam AC. Calculate the angle of tilt of the beam when it is subjectedto load P = 60 kN. The diameter of the strut is 50 mm and the diameter of the column is 80 mm.Answer: θ = 0.327 degreesPlease indicate the location of the angle of tilt in the FBD.
How to make a effective stiffness matrix for this figure?

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Q1 For the composite beam shown in fig. 1. Draw bending stress distribution .if E₁= 20 000 MPa., E22000 MPa. E1 20 000 MPa 20 MM- MATERIAL 1 E2 2000 MPa 10 kN A -4 M B 50 MM MATERIAL 2 100 MM -2 M -200 MM-