Analyze the given structure below using consistent deformation method. Show complete solution Determine the support reactions and internal member forces for the structure. E-200GPA A=2500 sqmm 3m 60KN 24 6m A 75KNV 8m

Analyze the given structure below using consistent deformation method. Show complete solution Determine the support reactions and internal member forces for the structure. E-200GPA A=2500 sqmm 3m 60KN 24 6m A 75KNV 8m

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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Matrix Algebra for Structural analysis

Structural analysis is a process in which the effects of different loads and internal forces, acting on structures and their elements are determined. This method of analysis is effective in detecting the failure loads of the structural elements and the design can be altered before commencing the construction process, which ensures proper strength and safety of the structures.

Question

Analyze the given structure below using consistent deformation method. Show complete solution
Determine the support reactions and internal member forces for the structure.
E=200GPA
A=2500 sqmm
24
3m
60KN
24
6m
A
75KNV
8m

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In a laboratory test of a beam loaded by end couples, the fiber at layer AB as shown are mm while those at CD decrease 70 x 10 mm in the 260- -3 found to increase 30 x 10 -3 mm-gage length. Using E = 150 GPa, determine the flexural stress at the bottom fiber. 40mm, b Answer must be in MPa. Given: a = = 110 mm, andc= 80 mm. gage length a mm b b mm c mm 8.
A load P will be supported by a structure consisting of a rigid bar ABCD, a polymer [E = 2,300 ksi; α = 2.9 × 10-6/°F] bar (1) and an aluminum alloy [E = 10,000 ksi; α = 12.5 × 10-6/°F] bar (2), as shown. Each bar has a cross-sectional area of 2.00 in.2. The bars are unstressed when the structure is assembled at 30°F. After a concentrated load of P = 56 kips is applied and the temperature is increased to 100°F, determine the normal force in bar (1).
A load P will be supported by a structure consisting of a rigid bar ABCD, a polymer [E = 2,300 ksi; a = 2.9 × 10-6/°F] bar (1) and an aluminum alloy [E = 10,000 ksi; a = 12.5 × 10-6/°F] bar (2), as shown. Each bar has a cross-sectional area of 2.00 in.². The bars are unstressed when the structure is assembled at 30°F. After a concentrated load of P = 69 kips is applied and the temperature is increased to 100°F, determine the normal force in bar (1). 6 ft 2.5 ft 07.01 kips 5.63 kips 8.39 kips 9.29 kips 6.66 kips (1) B 3 ft C 8 ft 1.5 ft