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Exam (elaborations)

Applied Strength of Materials – Seventh Edition by Robert L. Mott & Joseph A. Untener – Complete Solution Manual (Chapters 1-14) provides detailed, step-by-step solutions aligned with the main text, covering direct and shear stresses, torsion, bending, de

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The Applied Strength of Materials (7th Edition) Solution Manual by Robert L. Mott and Joseph A. Untener is a comprehensive companion resource for students and instructors using the main textbook. With the seventh edition of the textbook widely adopted in engineering technology programs, this solution manual offers fully worked-out solutions for all end-of-chapter problems (Chapters 1 through 14), allowing both verification of answers and deep insight into the methodology behind each solution. Each chapter in the main text focuses on an essential topic in strength of materials — from the foundational “Big Picture” overview of stresses and strains, through torsional deformation, shearing forces and bending in beams, centroids and moments of inertia, deflection of beams, combined stresses, columns and buckling, pressure vessel design, connection design, and thermal effects in composite elements. The solution manual mirrors that structure, offering step-by-step derivations, commentary on assumptions, unit conversions, typical engineering approximations, and design-oriented discussion where applicable. For students, the solution manual provides a powerful tool for self-study and exam preparation. When faced with a challenging problem, the student can attempt the problem independently, then consult the manual to compare their approach, identify gaps in their understanding, and reinforce correct problem-solving habits. The solutions help clarify when to apply direct stress versus shear stress formulas, how to evaluate torsional deformation, when to consider combined loading, how to calculate deflections in beams, and how to judge design criteria for columns or pressure vessels. The manual’s emphasis on engineering context also helps bridge the gap between mere calculation and practical engineering reasoning. For instructors, the manual becomes a ready resource for homework verification, assignment design, exam question formulation, and solution checking. Having a complete set of solutions allows instructors to focus more on pedagogical design rather than writing full solutions themselves. It also helps standardize grading and reduce ambiguity in student responses. One of the key strengths of this solution manual is its alignment with the "active learning" and design-oriented pedagogy emphasized in the seventh edition of the textbook. The text itself includes “Big Picture” introductions, real-world examples from civil and mechanical engineering, and a strong visual component. Barnes & Noble +2 +2 The manual complements these features by explaining the reasoning behind each step, showing multiple solution paths when relevant, and reinforcing conceptual understanding alongside computation. In summary, if you are using Applied Strength of Materials (7th Edition) as part of your course, this solution manual offers a full, professionally written guide to all the homework problems — making it an excellent investment for study, review, or teaching. It supports deeper understanding, better performance, and more effective learning in strength of materials and mechanics of materials courses.

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@SOLUTIONSSTUDY

Covers All 13 Chapters




SOLUTIONS MANUAL

,Chapter 1 Basic Concepts in Strength of Materials
1.1 to 1.15 Answers in text.
1.16 𝑊 = 𝑚 ∙ 𝑔 = 1800 kg ∙ 9.81 m/s2 = 17 658 (kg ∙ m)/s2 = 17 × 103 N
𝑾 = 𝟏𝟕. 𝟕 𝐤𝐍
1.17 Total Weight = 𝑚 𝑔 = 4000 kg ∙ 9.81 m/s2 = 39.24 kN

Each Front Wheel: 𝐹𝐹 = (1)2(0.40)(39.24 kN) = 𝟕. 𝟖𝟓 𝐤𝐍

Each Rear Wheel: 𝐹𝑅 = (1) (0.60)(39.24 kN) = 𝟏𝟏. 𝟕𝟕 𝐤𝐍
2

1.18 Loading = Total Force / Area
Total Force = 𝑚 𝑔 = 6800 kg ∙ 9.81 m/s2 = 66.7 kN
Area = (5.0 m)(3.5 m) = 17.5 m2
Loading = 66.7 kN⁄17.5 m2 = 3.81 kN⁄m2 = 𝟑. 𝟖𝟏 𝐤𝐏𝐚
1.19 Force = Weight = 𝑚 𝑔 = 25 kg ∙ 9.81 m/s2 = 245 N
K = Spring Scale = 4500 N⁄m = 𝐹/Δ𝐿
Δ𝐿 =
𝐹
=
245 N = 0.0545 m = 54.5 × 10−3 m = 𝟓𝟒. 𝟓 𝐦𝐦
𝐾 4500 N/m

1.22 𝑊 = 17.7 kN = 17 700 N ∙ 0.2248 (lb⁄N) = 𝟑𝟗𝟖𝟎 𝐥𝐛
1.23 𝐹𝐹 = 7.85 kN = 7850 N ∙ 0.2248 (lb⁄N) = 𝟏𝟕𝟔𝟓 𝐥𝐛
𝐹𝑅 = 11.77 kN = 11 770 N ∙ 0.2248 (lb⁄N) = 𝟐𝟔𝟒𝟔 𝐥𝐛
3 2
3.81×10 N
1.24 Loading = 3.81 kPa = × 0.2248 lb × 1m
= 𝟕𝟗 𝐥𝐛
m2 N (3.28 ft)2 𝐟𝐭𝟐

1.25 𝐹 = 245 N ∙ 0.2248 (lb⁄N) = 𝟓𝟓. 𝟏 𝐥𝐛
4500 N 0.2248 lb 1m = 𝟐𝟓. 𝟕 𝐥𝐛
𝐾= × ×
m N 39.37 in 𝐢𝐧
𝐹 55.1 lb = 𝟐. 𝟏𝟒 𝐢𝐧
Δ𝐿 = =
𝐾 25.7 (lb⁄in)
2
lb∙s
1.26 𝑚=
𝑤
=
2750 lb = 85.4 = 𝟖𝟓. 𝟒 𝐬𝐥𝐮𝐠𝐬
𝑔 32.2 (ft/s2) ft
2
lb∙s
1.27 𝑚=
𝑤
=
12800 lb = 398 = 𝟑𝟗𝟖 𝐬𝐥𝐮𝐠𝐬
𝑔 32.2 (ft/s2) ft

1.29 𝑝 = 1200 psi ∙ 6.895 (kPa⁄psi) = 𝟖𝟐𝟕𝟒 𝐤𝐏𝐚
1.30 𝜎 = 21 600 psi ∙ 6.895 (kPa⁄psi) = 149 000 kPa = 𝟏𝟒𝟗 𝐌𝐏𝐚

, @SOLUTIONSSTUDY




1.31 𝑠𝑢 = 14 000 psi ∙ 6.895 (kPa⁄psi) = 96 500 kPa = 𝟗𝟔. 𝟓 𝐌𝐏𝐚
𝑠𝑢 = 76 000 psi ∙ 6.895 (kPa⁄psi) = 524 000 kPa = 𝟓𝟐𝟒 𝐌𝐏𝐚
1750 rev 2π rad 1 min 𝐫𝐚𝐝
1.32 𝑛= × × = 𝟏𝟖𝟑
min rev 60s 𝐬
2
1.33 𝐴 = 14.1 in2 × (25.4 mm) = 𝟗𝟎𝟗𝟕 𝐦𝐦𝟐
in 2

1.34 𝑦 = 0.08 in ∙ 25.4 (mm⁄in) = 𝟐. 𝟎𝟑 𝐦𝐦
1.35 Dimensions: 18 in × 25.4 (mm/in) = 457 mm
12 in × 25.4 (mm/in) = 305 mm
Area = (18 in)2 = 𝟑𝟐𝟒 𝐢𝐧𝟐
Area = (457 mm)2 = 𝟐. 𝟎𝟗 × 𝟏𝟎𝟓 𝐦𝐦𝟐
Volume = 𝑉 = Area × Height
𝑉 = 324 in2 × 12 in = 𝟑𝟖𝟖𝟖 𝐢𝐧𝟑
𝑉 = (1.5 ft)2 × 1.0 ft = 𝟐. 𝟐𝟓 𝐟𝐭𝟑
𝑉 = (209 × 103 mm2) × 305 mm = 𝟔. 𝟑𝟕 × 𝟏𝟎𝟕 𝐦𝐦𝟑
𝑉 = (0.457 m)2 × 0.305 m = 0.0637 m3 = 𝟔. 𝟑𝟕 × 𝟏𝟎−𝟐 𝐦𝟑
1.36 𝐴 = 𝜋𝐷2⁄4 = 𝜋(0.505 in)2⁄4 = 𝟎. 𝟐𝟎𝟎 𝐢𝐧𝟐
2
𝐴 = 0.200 in2 × (25.4 mm) = 𝟏𝟐𝟗 𝐦𝐦𝟐
in 2
3200 N N
1.37 𝜎=𝑃= =
3200 N = 40.7 = 𝟒𝟎. 𝟕 𝐌𝐏𝐚
𝐴 (𝜋𝐷2⁄4) [𝜋(10 mm) 2]⁄4 mm2

𝑃 20×10 3 N = 66.7 N
= 𝟔𝟔. 𝟕 𝐌𝐏𝐚
1.38 𝜎= =
𝐴 (10)(30) mm2 mm2
860 lb
1.39 𝜎=𝑃= = 𝟓𝟑𝟕𝟓 𝐩𝐬𝐢
𝐴 (0.40 in)2
𝑃 1850 lb = 𝟏𝟔 𝟕𝟓𝟎 𝐩𝐬𝐢
1.40 𝜎= =
𝐴 [𝜋(0.375 in)2]⁄4

1.41 Load on Shelf = 𝑊 = 𝑚𝑔 = 1840 kg ∙ 9.81 m⁄s2 = 18 050 N
𝑊/2 = 9025 N On each side
∑ 𝑀𝐴 = 0 = (9025 N)(600 mm) − 𝐶𝑉(1200 mm)
𝐶𝑉 = 4512 N
𝐶 = 𝐶𝑉/ sin 30° = 9025 N
𝑃 𝐶 9025 N = 𝟕𝟗. 𝟖 𝐌𝐏𝐚
𝜎= = =
𝐴 𝐴 [𝜋(12 mm) 2]⁄4
𝑃 70000 lb = 𝟏𝟑𝟗𝟑 𝐩𝐬𝐢
1.42 𝜎= =
𝐴 [𝜋(8 in)2]/4

, (29500 lb)/3
1.43 𝜎= 𝑃 = = 𝟖𝟎𝟑 𝐩𝐬𝐢
𝐴 (3.5 in)2
3500 N
1.44 𝜎=𝑃= = 𝟓𝟒. 𝟕 𝐌𝐏𝐚
𝐴 (8.0 mm)2

1.45 𝑊 = 𝑚 𝑔 = 4200 kg ∙ 9.81 m/s2 = 41.2 kN
𝐴𝐵𝑋 = 𝐴𝐵 sin 35°
𝐴𝐵𝑌 = 𝐴𝐵 cos 35°
𝐵𝐶𝑋 = 𝐵𝐶 sin 55°
𝐵𝐶𝑌 = 𝐵𝐶 cos 55°
∑ 𝐹𝑋 = 0 = 𝐴𝐵𝑋 − 𝐵𝐶𝑋
0 = 𝐴𝐵 sin 35° − 𝐵𝐶 sin 55°
sin 55°
𝐴𝐵 = 𝐵𝐶 ∙ = 1.428 𝐵𝐶 sin
35°
∑ 𝐹𝑉 = 0 = 𝐴𝐵𝑌 + 𝐵𝐶𝑌 − 41.2 kN = 𝐴𝐵 cos 35° + 𝐵𝐶 cos 55° − 41.2 kN 0
= (1.428 𝐵𝐶) cos 35° + 𝐵𝐶 cos 55° − 41.2 kN
41.2 kN = 𝐵𝐶[1.170 + 0.574] = 1.743 𝐵𝐶
41.2 kN
𝐵𝐶 = = 23.63 kN
1.743

𝐴𝐵 = 1.428 𝐵𝐶 = 33.75 kN
Stress in Rod AB: 𝜎 =
𝐴𝐵
=
33.75×10 3 N = 𝟏𝟎𝟕. 𝟒 𝐌𝐏𝐚
𝐴𝐵 𝐴 [𝜋(20 mm) 2]/4

Stress in Rod BC: 𝜎 =
𝐵𝐶
=
23.63×10 3 N = 𝟕𝟓. 𝟐 𝐌𝐏𝐚
𝐵𝐶 𝐴 [𝜋(20 mm) 2]/4

Stress in Rod BD: 𝜎 =
𝐵𝐷
=
41.2×10 3 N = 𝟏𝟑𝟏. 𝟏 𝐌𝐏𝐚
𝐵𝐷 𝐴 [𝜋(20 mm) 2]/4

1.46 𝐹 = 0.01097 𝑚 𝑅 𝑛2 = (0.01097)(0.40)(0.60)(3000)2 N
𝐹 = 23 695 N
𝜋(16 mm)2
𝐴= = 201 mm2
4
𝐹 23695 N = 𝟏𝟏𝟖 𝐌𝐏𝐚
𝜎= =
𝐴 201 mm2

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