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Solutions Manual for Structural Steel Design (3rd Edition) by Abi Aghayere & Jason Vigil – Complete Step-by-Step Worked Solutions for Steel Structure Analysis and Design Using AISC, Load Calculations, Beam Design, Column Design, Bolted & Welded Connection

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This Solutions Manual for Structural Steel Design (3rd Edition) by Abi Aghayere & Jason Vigil provides complete, step-by-step worked solutions to all exercises in the textbook. It is ideal for students, instructors, and structural engineering professionals who want clear, verified solutions based on the latest AISC steel design provisions. This manual breaks down every problem logically, showing all formulas, diagrams, equations, and final answers used in structural steel design. Topics include tension members, compression members, beams, composite structures, bolted and welded connections, load combinations, LRFD/ASD design methods, bracing, and plate girder design. Whether you're preparing assignments, reviewing for exams, or designing steel structures in practice, this manual serves as an excellent guide for mastering structural steel design concepts with confidence. WHAT’S INCLUDED Full Solutions Manual in PDF Step-by-step solutions to all textbook problems Covers LRFD & ASD methods AISC-based calculations Diagrams, equations, & clear explanations Perfect for homework, exams, or self-study Instant digital reference for structural engineers WHO IS THIS FOR? This manual is ideal for: Civil & Structural Engineering Students University Instructors / TAs EIT/FE Exam Preparation Structural Engineering Professionals Steel Design Coursework (AISC-based programs)

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@SOLUTIONSSTUDY


All 13 Chapters Covered




SOLUTIONS

, @SOLUTIONSSTUDY


Contents
Chapter 1 .................................................................................................................................... 1

Chapter 2 .................................................................................................................................... 6

Chapter 3 .................................................................................................................................... 23

Chapter 4 .................................................................................................................................... 41

Chapter 5 .................................................................................................................................... 55

Chapter 6 .................................................................................................................................... 62

Chapter 7 .................................................................................................................................... 74

Chapter 8 .................................................................................................................................... 84

Chapter 9 .................................................................................................................................... 92

Chapter 10 .................................................................................................................................. 109

Chapter 11 .................................................................................................................................. 119

Chapter 12 .................................................................................................................................. 137

Chapter 13 .................................................................................................................................. 154

Appendix B.................................................................................................................................. 159

, @SOLUTIONSSTUDY


Problem 1-4

The size and cross-sectional areas are obtained from Part 1 of the AISCM as follows:

Size Self-weight (lb/ft.) Cross-sectional area (in2)
W14x22 22 6.49
W21x44 44 13.0
HSS 6x6x½ 35.11 9.74
L6x4x½ 16.2 4.75
C12x30 30 8.81
WT18x128 128 37.7


Problem 1-5

a)

Element A y Ay I d = y- y I + Ad2

top flange 21 26.25 551.25 3.94 -12.75 3418
web 21 13.5 283.5 1008 0 1008
bot flange 21 0.75 15.75 3.94 12.75 3418
= 63 in.2 850.5 I = 7844 in.4

Ay 850.5
y = 13.5 in.
A 63
Self weight = (63/144)(490 lb/ft3) = 214 lb/ft.


b)

Element A y Ay I d = y- y I + Ad2

top plate 2.63 18.26 47.93 0.03 -9.04 214.3
beam 10.3 9.23 95.02 510 0 510
bot plate 2.63 0.188 0.49 0.03 9.04 214.3
= 15.55 in.2 143.4 I = 939 in.4

Ay 143.4
y = 9.23 in.
A 15.55
Self weight = (15.55/144)(490 lb/ft3) = 52.9 lb/ft.


c) From AISCM Table 1-20, Ix = 314 in.4
Area = 13.8 in2
Self weight = 47.1 lb/ft.

, @SOLUTIONSSTUDY


Problem 1-7

Plot the idealized stress-strain diagram for a 6-in. wide by ½-in. thick plate and a 6-in. wide by
1-in. thick plate of ASTM A36 steel. Assume that the original length between two points on the
specimen over which the elongation will be measured (i.e. the gage length) is 2-in.

Solution:

Gage length, Lo = 2 in.
For 6 x ½-in. plate, Area = (6 in.)(½ in.) = 3
in2 E = 29,000 ksi

P Stress = P/A Strain, = P/EA Elongation, Lo = Strain x gage length = Lo

(kips) (ksi) (in.)
0 0 0 0
20 6.67 0.00023 0.00046
40 13.33 0.00046 0.00092
60 20.0 0.00069 0.00138
80 26.67 0.00092 0.00184
100 33.33 0.00111 0.00222
108 36.0 0.00124 0.00248




For 6 x 1-in. plate, Area = (6 in.)(1 in.) = 6 in2

P Stress = P/A Strain, = P/EA Elongation, Lo = Strain x gage length = Lo

(kips) (ksi) (in.)
0 0 0 0
40 6.67 0.00023 0.00046
80 13.33 0.00046 0.00092
120 20.0 0.00069 0.00138
160 26.67 0.00092 0.00184
200 33.33 0.00111 0.00222
216 36.0 0.00124 0.00248


Problem 1-8

Determine the most economical layout of the roof framing (joists and girders) and the gage
(thickness) of the roof deck for a building with a 25 ft x 35 ft typical bay size. The total roof dead
load is 25 psf and the snow load is 35 psf. Assume a 1½” deep galvanized wide rib deck and an
estimated weight of roof framing of 6 psf.

*Assume beams (or joists) span the 35’ direction

Información del documento

Subido en
24 de octubre de 2025
Número de páginas
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Escrito en
2025/2026
Tipo
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