A = 4B = 0C = 7Show complete solution. For the given structural steel sections below, determine the following:a. The location of the centroid from the given X and Y-axesb. The centroidal moments of inertia Igx and Igyc. The section moduli Sx and Syd. The polar moment of inertia, Je. The radius of gyration rx and ry 5. Channel section and angular section with longer leg verticalNote: A, B and C are the last 3 digits of your student number.Ex. Student Number 2015140962 "A"=9; "B"=6; "C"=2"A"0123456789Channel SectionC 9x20C 9x13.4C 9x15C 8x18.75C 8x13.75C 8x11.5C 7x14.75C 7x12.25C 7x9.8C 6x13"B" Wide Flange Section "C"0W10x68W10x60W10x54W10x49W10x45W10x39W10x33123456[789W10x30W10x26W10x220123456789Angle SectionL6x4x7/8L6x4x 3/4L6x4x5/8L6x4x9/16L6x4x1/2L6x4x7/16L6x4x3/8L6x4x5/16L6x3.5x1/2L6x3.5x3/8

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For the given structural steel sections below, determine the following: a. The location of the centroid from the given X and Y-axes b. The centroidal moments of inertia Igx and Igy c. The section moduli Sx and Sy d. The polar moment of inertia, J e. The radius of gyration rx and ry

For the given structural steel sections below, determine the following: a. The location of the centroid from the given X and Y-axes b. The centroidal moments of inertia Igx and Igy c. The section moduli Sx and Sy d. The polar moment of inertia, J e. The radius of gyration rx and ry

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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Question

A = 4

B = 0

C = 7

Show complete solution.

For the given structural steel sections below, determine the following:
a. The location of the centroid from the given X and Y-axes
b. The centroidal moments of inertia Igx and Igy
c. The section moduli Sx and Sy
d. The polar moment of inertia, J
e. The radius of gyration rx and ry

5. Channel section and angular section with longer leg vertical
Note: A, B and C are the last 3 digits of your student number.
Ex. Student Number 2015140962 "A"=9; "B"=6; "C"=2
"A"
0
1
2
3
4
5
6
7
8
9
Channel Section
C 9x20
C 9x13.4
C 9x15
C 8x18.75
C 8x13.75
C 8x11.5
C 7x14.75
C 7x12.25
C 7x9.8
C 6x13
"B" Wide Flange Section "C"
0
W10x68
W10x60
W10x54
W10x49
W10x45
W10x39
W10x33
1
2
3
4
5
6
[
7
8
9
W10x30
W10x26
W10x22
0
1
2
3
4
5
6
7
8
9
Angle Section
L6x4x7/8
L6x4x 3/4
L6x4x5/8
L6x4x9/16
L6x4x1/2
L6x4x7/16
L6x4x3/8
L6x4x5/16
L6x3.5x1/2
L6x3.5x3/8

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given data

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determination of section properties

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determination of centroid of given section

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determination of centroidal moment of inertia

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determination of section modulii

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determination of polar moment of inertia

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determination of radius of gyration

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