a 36 ull AsiacelIاسئلة ت مواد.pdf>Q1: Find the normal stresses at sections A-A, B-B, C-C, and, D-D for thebody as shown in figure (1).60 KNBD=60mmD=150mm82kND=30mm32kN50KN60KNBCDFigure (1)Q3: For the body shown in figure (2). Determine the normal stresses atsections A-A, B-B, C-C, and D-DAD60KN45D=100mmD=50mm80KND=25mm32kN48KNA4560KNВCFigure (2)Q3 - Find the normal stress at sections A-A, B-B, C-C, and D-D forthe member shown in Figure (3). A assume that thearea of the member is (A mm²) , and the weight of member is (W kN )cross sectional

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QI: Find the normal stresses at sections A-A, B-B, C-C, and, D-D for the body as shown in figure (1). 60 KN D A B D=60mm D=150mm 82kN D=30mm 32kN 50KN A 60kN в C D

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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Types and properties of steel

Steel is an alloy of iron. It is formed by heating iron and combining carbon (0.1-1.7%) with it and minor amounts of other elements such sulfur, chromium, manganese, nickel, etc. Thousands of steel grades have been published, registered, or regulated around the world, each with its chemical composition, and special numbering systems have been devised in various countries to classify the vast number of alloys.

Question

a 36 ull AsiacelI
اسئلة ت مواد.pdf
>
Q1: Find the normal stresses at sections A-A, B-B, C-C, and, D-D for the
body as shown in figure (1).
60 KN
B
D=60mm
D=150mm
82kN
D=30mm
32kN
50KN
60KN
B
C
D
Figure (1)
Q3: For the body shown in figure (2). Determine the normal stresses at
sections A-A, B-B, C-C, and D-D
A
D
60KN
45
D=100mm
D=50mm
80KN
D=25mm
32kN
48KN
A
45
60KN
В
C
Figure (2)
Q3 - Find the normal stress at sections A-A, B-B, C-C, and D-D for
the member shown in Figure (3). A assume that the
area of the member is (A mm²) , and the weight of member is (W kN )
cross sectional

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