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Applied Strength of Materials (6th Edition) SI Units Version – Solution Manual by Robert L. Mott & Joseph A. Untener (2018) – A complete companion manual providing fully-worked solutions for each chapter covering basic concepts, design properties of mater

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The Applied Strength of Materials (6th Edition) SI Units Version – Solution Manual by Robert L. Mott and Joseph A. Untener is an indispensable companion for students and instructors alike who use the SI-units version of the primary textbook. With all chapters addressed in the main text, this manual presents fully worked solutions to the end-of-chapter problems — not just final answers, but detailed step-by-step derivations, clear reasoning, consistent SI-unit usage, and design-oriented commentary. Structured to mirror the textbook’s chapter flow, the manual begins with basic concepts of strength of materials — covering unit systems, stress and strain, and the fundamental variables engineers must understand. It then progresses through material design properties (metals, composites, non-metals), direct stress and deformation members, shear and torsional deformation, bending and shear in beams, combined stresses, columns, and also special topics such as pressure vessels and connections. Each section isn’t merely about plugging into formulas, but about interpreting results, applying design guidelines, and understanding what the numbers imply in practice. What sets this solution manual apart is its rigorous emphasis on design context. Since the main text integrates both analysis and design of mechanical and structural members, the manual similarly explains not only how to compute stress, strain or deflection, but how to select appropriate factors of safety, consider material choices, and check against realistic service criteria. This makes it ideal for engineering-technology programs where students must bridge textbook theory with real-world application. The manual’s exclusive use of SI units ensures global applicability — whether for courses in Europe, Asia, or elsewhere where SI units dominate. The step-by-step solutions also cater to self-study: a student stuck on a torsion problem can follow the manual’s approach, compare methods (for example, pure torsion vs combined loading), and gain confidence through repeated modeled examples before attempting novel problems. For instructors, it offers a transparent solution source, enabling efficient creation of assignments, labs, or exams, while preserving academic integrity by varying problem parameters if desired. Within the engineering curriculum, the manual serves multiple roles: as a homework-check resource, an exam-preparation guide, and a refresher tool for those revisiting mechanics of materials after a break. It also supports students who may struggle with the leap from statics to strength of materials by providing granular explanations of each step — what assumptions are made, why factor of safety is chosen certain way, how to interpret the results from a design viewpoint. In summary, the Applied Strength of Materials (6th Edition) SI Units Version – Solution Manual is more than “answers only.” It is a rich pedagogical tool that fosters learning, supports teaching, and enhances engineering reasoning in the domain of strength of materials. If you’re using the SI-units version of the main text and want a detailed, design-aware solution manual, this is a top choice

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Food Chemistry
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October 31, 2025
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,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
1
Each Front Wheel: 𝐹𝐹 = ( )2 (0.40)( 39.24 kN) = 𝟕. 𝟖𝟓 𝐤𝐍
1
Each Rear Wheel: 𝐹𝑅 = ( )2 (0.60)( 39.24 kN) = 𝟏𝟏. 𝟕𝟕 𝐤𝐍

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
𝑃 3200 N N
1.22 𝜎= = =
3200 N = 40.7 = 𝟒𝟎. 𝟕 𝐌𝐏𝐚
𝐴 (𝜋𝐷2⁄4) [𝜋(10 mm) 2]⁄4 mm2

𝑃 20×10 3 N N
1.23 𝜎= = = 66.7 = 𝟔𝟔. 𝟕 𝐌𝐏𝐚
𝐴 (10)(30) mm2 mm2


𝑃 3500 N
1.24 𝜎= = = 𝟑𝟓. 𝟎 𝐌𝐏𝐚
𝐴 (0.010 m)2
𝑃 8300 N
1.25 𝜎= = = 𝟏𝟑𝟎. 𝟓 𝐌𝐏𝐚
𝐴 [𝜋(9.0 mm)2]⁄4



1.26 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




@SOLUTIONSSTUDY

, 𝑃 310×10 3 N = 𝟗. 𝟖𝟕 𝐌𝐏𝐚
1.27 𝜎= =
𝐴 [𝜋(0.2 m) 2]/4


𝑃 (132 000 N)/3
1.28 𝜎= = = 𝟔. 𝟏 𝐌𝐏𝐚
𝐴 (85 mm)2
𝑃 3500 N
1.29 𝜎= = = 𝟓𝟒. 𝟕 𝐌𝐏𝐚
𝐴 (8.0 mm)2

1.30 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



1.31 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

, 1.32 𝐴 = (30 mm)2 = 900 mm2
For AB: 𝐹𝐴𝐵 = (110 − 40 + 80) kN = 150 kN
𝐹𝐴𝐵 150×103 N
𝜎 = = = 𝟏𝟔𝟕 𝐌𝐏𝐚 Tension
𝐴𝐵 𝐴 900 mm2

For BC: 𝐹𝐵𝐶 = 110 − 40 = 70 kN
𝐹𝐵𝐶 70×103 N
𝜎 = = = 𝟕𝟕. 𝟖 𝐌𝐏𝐚 Tension
𝐵𝐶 𝐴 900 mm2

For CD: 𝐹𝐶𝐷 = 110 kN
𝐹𝐶𝐷 110×103 N
𝜎 = = = 𝟏𝟐𝟐 𝐌𝐏𝐚 Tension
𝐶𝐷 𝐴 900 mm2



1.33 Areas: A-C; 𝐴1 = 𝜋(25)2/4 = 491 mm2
C-D; 𝐴2 = 𝜋(16)2/4 = 201 mm2
For AB: 𝐹𝐴𝐵 = −9.65 − 12.32 + 4.45 = −17.52 kN
𝐹𝐴𝐵 −17.52×103 N
𝜎 = = = −𝟑𝟓. 𝟕 𝐌𝐏𝐚 Compression
𝐴𝐵 𝐴1 491 mm2

For BC: 𝐹𝐵𝐶 = −9.65 − 12.32 = −21.97 kN
𝐹𝐵𝐶 −21.97×103 N
𝜎 = = = −𝟒𝟒. 𝟕 𝐌𝐏𝐚 Compression
𝐵𝐶 𝐴1 491 mm2

For CD: 𝐹𝐶𝐷 = −9.65 kN
𝐹𝐶𝐷 −9.65×103 N
𝜎 = = = −𝟒𝟖. 𝟎 𝐌𝐏𝐚 Compression
𝐶𝐷 𝐴2 201 mm2



1.34 𝐴 = 515.8 mm2 [𝐷𝑁 40 Pipe-Appendix A-9(b)]
For BC: 𝜎 =
𝐹𝐵𝐶
=
11 000 N = 𝟐𝟏. 𝟑 𝐌𝐏𝐚 Tension
𝐵𝐶 𝐴 515.8 mm2

For AB: 𝐹𝐴𝐵 = 11 000 + 2(36 000 cos 30°) = 73 354 N
𝜎𝐴𝐵 =
𝐹𝐴𝐵
=
73 354 N = 𝟏𝟒𝟐. 𝟐 𝐌𝐏𝐚 Tension
𝐴 515.8 mm



1.35 ∑ 𝑀𝐶 = 0 = 13 000 N(1.2 m) − 𝐹𝐵𝐷(0.8)
𝐹𝐵𝐷 = 19 500 N
𝜎𝐵𝐷 =
𝐹𝐵𝐷
=
19 500 N = 𝟒𝟖. 𝟖 𝐌𝐏𝐚 Tension
𝐴 (25)(16) mm2




@SOLUTIONSSTUDY

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