Compute the moment of inertia for the built up sectionshown below about the strong axis only. (Group 2)½"x 4"WebFlangeDistanceArea, Depth,Work-k T ableGagekThickness,2Thickness,Width,brShapeAKdes Kartin.7.64 7%8 0.810 13/16 1.21 121.15 1/16in.?in.in.in.in.in.in.in.in.in./% 152 32W18x71x65x60x55°x5020.9 18.5 1820.495 219.1 18.4 18% 0.450 1617.6 18.2 184 0.415 /1616.2 18.1 18e 0.390 3814.7 18.0 18 0.355 %%7.59 7%s 0.750 347/813/1613/167.56 72 0.695 /16 1.10 116 7.53 72 0.630 %8 1.03 1%1613/1616 7.50 72 0.570 16 0.972 14W18 × 65CompactNom- SectioninalTorsionalAxis X-XAxis Y-YPropertiesCriteriahoWt.byIb/ft 2t71 4.71 32.4 117065 5.06 35.7 107060 5.44 38.755 5.98 41.150 6.57 45.2CwSin.in. in.in.127117in.in.60.354.8in.15.8 1.70 24.714.4 1.6913.3 1.68 20.6in.3.49in.in.7.50 1467.49 1337.47 1237.41 112in.in.2.05 17.722.5 2.03 17.72.02 17.52.00 17.51.98 17.447002.73424098410850.12.17385089098.344.911.9 1.6718.51.66343080088.9 7.38 10140.110.7 1.6516.61.243040

Answered: Image /qna-images/answer/493a30c1-e9d7-4b20-945d-499b0827d763.jpg

7.59 7% 0.750 1.15 1% % Compute the moment of inertia for the built up section shown below about the strong axis only. (Group 2) - ½"x 4" I. Web Flange Distance Area, Depth, Work- able Gage k Thickness, 2 Width, Thickness, Shape A ki Kdes kart in.? in. in. in. in. in. in. in. in. in. in. W18x71 x65 x60° x55 20.9 18.5 182 0.495 2 19.1 18.4 18 0.450 /16 17.6 18.2 1840.415 /16 4 16.2 18.1 18% 0.390 /8 14.7 18.0 18 0.355 %% 7.64 7% 0.810 13/16 1.21 12 14 7.56 72 0.695 /16 1.10 1% 316 7.53 72 0.630 %8 1.03 1%16 13/16 /16 7.50 72 0.570 16 0.972 14 /8 152 32 1/16 13/18 x50 13/16 W18 x 65 Compact Nom- Section inal Wt. Torsional Axis X-X Axis Y-Y Properties Criteria ho J Cw S Ib/ft 2t in. in. in. in. 60.3 in. in. in. 3.49 in. 4700 in. 15.8 1.70 24.7 54.8 14.4 1.69 22.5 13.3 1.68 20.6 11.9 1.67 18.5 10.7 1.65 in. in. 2.05 17.7 2.03 17.7 2.02 17.5 2.00 17.5 1.98 17.4 in. 71 4.71 32.4 1170 65 5.06 35.7 1070 60 5.44 38.7 55 5.98 41.1 50 6.57 45.2 7.50 146 7.49 133 7.47 123 98.3 7.41 112 88.9 7.38 101 127 117 2.73 4240 984 108 50.1 2.17 3850 890 800 44.9 1.66 3430 3040 40.1 16.6 1.24

7.59 7% 0.750 1.15 1% % Compute the moment of inertia for the built up section shown below about the strong axis only. (Group 2) - ½"x 4" I. Web Flange Distance Area, Depth, Work- able Gage k Thickness, 2 Width, Thickness, Shape A ki Kdes kart in.? in. in. in. in. in. in. in. in. in. in. W18x71 x65 x60° x55 20.9 18.5 182 0.495 2 19.1 18.4 18 0.450 /16 17.6 18.2 1840.415 /16 4 16.2 18.1 18% 0.390 /8 14.7 18.0 18 0.355 %% 7.64 7% 0.810 13/16 1.21 12 14 7.56 72 0.695 /16 1.10 1% 316 7.53 72 0.630 %8 1.03 1%16 13/16 /16 7.50 72 0.570 16 0.972 14 /8 152 32 1/16 13/18 x50 13/16 W18 x 65 Compact Nom- Section inal Wt. Torsional Axis X-X Axis Y-Y Properties Criteria ho J Cw S Ib/ft 2t in. in. in. in. 60.3 in. in. in. 3.49 in. 4700 in. 15.8 1.70 24.7 54.8 14.4 1.69 22.5 13.3 1.68 20.6 11.9 1.67 18.5 10.7 1.65 in. in. 2.05 17.7 2.03 17.7 2.02 17.5 2.00 17.5 1.98 17.4 in. 71 4.71 32.4 1170 65 5.06 35.7 1070 60 5.44 38.7 55 5.98 41.1 50 6.57 45.2 7.50 146 7.49 133 7.47 123 98.3 7.41 112 88.9 7.38 101 127 117 2.73 4240 984 108 50.1 2.17 3850 890 800 44.9 1.66 3430 3040 40.1 16.6 1.24

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: The frame given in the figure R = 0.25m radius at point E a frictionless reel are available. Support…

Q: The assembly consists of two 10-mm diameter red brass C83400 copper rods AB and CD, a 15- mm…

A: Given data : To Find :

Q: Evaluate the following limit Lim X-X r-2 4. o N

Q: 5 ft 7.84 Find the smallest angle B for which the uniform crate can be tipped about corner A. Also…

A: Show the free body diagram of the uniform crate as in Figure (1).

Q: Like/Thumbs-up

Q: 2 - Reflect & comment on how would you solve the problem if the system is subjected to ground…

A: Answer If the system is subjected to ground motion, we will use the formula F=-Kx and, while acting…

Q: 3. A plate is held against a horizontal water jet in the horizontal plane as shown. The jet has a…

A: Given data:- The diameter of the jet (d), d=30 mm=0.03 m The given force required to hold the plate…

Q: Determine the AV (change in volume) of the 8-in. length of the rod shown if the rod is made of steel…

A: The basic relation between bulk modulus and young's modulus is E = 3K1-2×μ29×106 =…

Q: 300 mm B 600 mm 400 N.m 600 mm 200 N·m 800 N·m The 50-mm-diameter A992 steel shaft is subjected to…

A: A solid shaft of diameter, d = 50 mm is given. To determine the angle of twist at end A. Modified…

Q: 4) While trying to change a tire, the driver shown below applies a force, P, of 25 Ibs at each end…

Q: * n 8.36 A structural steel built-up section is fabricated as shown. Calculate (a) the moments of…

Q: 1- Calculate maximum deflection of the beams. 2- Check the suitability of the section assuming the…

A: UKB 457 x 152 x 82 I = 366,000,000 mm4 E = 2 x 105 FIND1- Calculate maximum deflection of the…

Q: Consider Figure P5-45 on P. 186 on your textbook. The distance between points A and B is 10 in and…

Q: DETERMINE THE STRETCH IN SPRING OC To SUPPORT THE SOD Ib LOAD. AUSO DETERNINZ THE TErSION FORLSS IN…

A: To determine the tension in all the cables and the stretch in the spring. From the given figure,…

Concept explainers

Introduction to Engineering Design

Students are often confused with engineering and design. The term engineering design has two words with different meanings, engineering, and design. The term engineering implies applications of laws and principles of science to design and analyze physical structures and components. In civil engineering, students apply the concept of physics and chemistry to design and build structures and buildings. In engineering disciplines, the term design means determining the dimensions, loads, and associated influences on the component due to the applied loads such as stresses and deformations. The estimation of such parameters is crucial to make the component or structure foolproof.

Question

Compute the moment of inertia for the built up section
shown below about the strong axis only. (Group 2)
½"x 4"
Web
Flange
Distance
Area, Depth,
Work-
k T able
Gage
k
Thickness,
2
Thickness,
Width,
br
Shape
A
Kdes Kart
in.
7.64 7%8 0.810 13/16 1.21 12
1.15 1/16
in.?
in.
in.
in.
in.
in.
in.
in.
in.
in.
/% 152 32
W18x71
x65
x60
x55°
x50
20.9 18.5 1820.495 2
19.1 18.4 18% 0.450 16
17.6 18.2 184 0.415 /16
16.2 18.1 18e 0.390 38
14.7 18.0 18 0.355 %%
7.59 7%s 0.750 34
7/8
13/16
13/16
7.56 72 0.695 /16 1.10 1
16 7.53 72 0.630 %8 1.03 1%16
13/16
16 7.50 72 0.570 16 0.972 14
W18 × 65
Compact
Nom- Section
inal
Torsional
Axis X-X
Axis Y-Y
Properties
Criteria
ho
Wt.
by
Ib/ft 2t
71 4.71 32.4 1170
65 5.06 35.7 1070
60 5.44 38.7
55 5.98 41.1
50 6.57 45.2
Cw
S
in.
in. in.
in.
127
117
in.
in.
60.3
54.8
in.
15.8 1.70 24.7
14.4 1.69
13.3 1.68 20.6
in.
3.49
in.
in.
7.50 146
7.49 133
7.47 123
7.41 112
in.
in.
2.05 17.7
22.5 2.03 17.7
2.02 17.5
2.00 17.5
1.98 17.4
4700
2.73
4240
984
108
50.1
2.17
3850
890
98.3
44.9
11.9 1.67
18.5
1.66
3430
800
88.9 7.38 101
40.1
10.7 1.65
16.6
1.24
3040

Expert Solution

Step 1

Trending now

This is a popular solution!

Step by step

Solved in 2 steps with 2 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.

Similar questions

Please read instructions carefully. Especially ”change the steel shaft from solid cross-section to tubular cross section’’.
For the beam and loading shown, calculate (a) the equation of the elastic curve, (b) the deflection at point B, (c) the deflection at point C. A | 12 B L./2 Wo IC X
What is the C or T, the X and Y components and the load of each member. Also can you put the answer like it is on the image.
how to solve this question step by step
how to solve the question attached
A horizontal beam ABC is loaded as shown in the figure below. The distance of the point of contraflexure from end A (in m) is 10kN (327) Ag 0.75m B C k D 1m -
Hhhhh
The tongs are used to lift the 150-kg crate, whose center of mass is at G. Determine which Free Body Diagram can be used to find the least coefficient of static friction at the pivot blocks so that the crate can be lifted. 500 mm 500 mm 275 mm LOS E 300 A H B
A cantilever beam shown in Fig, with rectangular section shown. Its carry uniform load wand concentrated load Pa=12 KN, F-0.5. a- Calculate the instantaneous and 6- years long-term deflections at free end b - Check the deflections with ACI-Code limitations. Pa 012 stirrups 66 29 2 29 K-bw fy bw, L W, kN/m? h, mm Wa mm 27 410 180 3.25 4.75 5.6 500
Please read instructions carefully.