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Exam (elaborations)

Solution Manual for Applied Strength of Materials (7th Edition, 2022) by Mott and Untener

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This complete solution manual provides detailed, step-by-step answers to all end-of-chapter problems in Applied Strength of Materials (7th Edition) by Robert L. Mott and Joseph A. Untener. Topics include stress and strain analysis, axial loading, torsion, shear and bending in beams, combined loading, stress transformation, deflection, and column buckling — all aligned with real-world engineering applications and design principles. Compiled from two merged files, this resource ensures full coverage of both metric and U.S. customary unit problems, making it an ideal study aid for coursework, homework help, and engineering exam prep. applied strength of materials solutions, mott 7th edition solution manual, mechanical engineering strength of materials, beam bending problems solved, shear force and moment diagrams, stress strain analysis answers, combined loading solutions, column buckling problems, material mechanics textbook answers, axial and torsional loading, civil engineering material strength, deflection of beams exercises, strength of materials homework help, mott untener 2022 answers, structural analysis solved examples

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Covers All 13 Chapters




SOLUTIONS MANUAL

,Chapter 1 Answers
1.1 to 1.15 Basic Concepts in Strength of Materials
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
1
kg ∙ 9.81 m/s2 = 39.24 kN
Each Front Wheel: 𝐹 = ( ) (0.40)(39.24 kN) = 𝟕. 𝟖𝟓 𝐤𝐍
𝐹 2
1
Each Rear Wheel: 𝐹 = ( ) (0.60)(39.24 kN) = 𝟏𝟏. 𝟕𝟕 𝐤𝐍
𝑅 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
= 0.0545 m = 54.5 × 10−3 m = 𝟓𝟒. 𝟓 𝐦𝐦
Δ𝐿 = =
245 N
𝐾 4500 N/m
1.22 𝑊 = 17.7 kN = 17 700 N ∙ 0.2248 (lb⁄N) = 𝟑𝟗𝟖𝟎 𝐥𝐛
1.23 𝐹 = 7.85 kN = 7850 N ∙ 0.2248 (lb⁄N) = 𝟏𝟕𝟔𝟓 𝐥𝐛

𝐹 = 11.77 kN = 11 770 N ∙ 0.2248 (lb⁄N) = 𝟐𝟔𝟒𝟔 𝐥𝐛
3.81×10 𝐥𝐛
1.24 Loading = 3.81 kPa = 3
N 0.2248 lb 1m
2
= 𝟕𝟗
× ×
m2 N (3.28 ft)2 𝐟𝐭𝟐

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




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,1.31 𝑠 = 14 000 psi ∙ 6.895 (kPa⁄psi) = 96 500 kPa = 𝟗𝟔. 𝟓 𝐌𝐏𝐚
𝑠 = 76 000 psi ∙ 6.895 (kPa⁄psi) = 524 000 kPa = 𝟓𝟐𝟒 𝐌𝐏𝐚
1750 rev 2π rad 1 min 𝐫𝐚𝐝
1.32 𝑛= × × =60s𝟏𝟖𝟑 𝐬
min (25.4rev
mm) 2
1.33 𝐴 = 14.1 in × 2

= 𝟗𝟎𝟗𝟕 𝐦𝐦𝟐
in2
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 = (0.505 in)22⁄4 = 𝟎. 𝟐𝟎𝟎 𝐢𝐧𝟐
(25.4 mm)
𝐴 = 0.200 in2 × = 𝟏𝟐𝟗 𝐦𝐦𝟐
in2
𝑃 3200 N N
1.37 𝜎= = 3200 N = 40.7 = 𝟒𝟎. 𝟕 𝐌𝐏𝐚
=
𝐴 (𝜋𝐷2⁄4) [(10 mm)2]⁄4 mm2
N
𝑃
3
20×10 N = 66.7 = 𝟔𝟔. 𝟕 𝐌𝐏𝐚
1.38 𝜎= =
𝐴 (10)(30) mm2 mm2
860 lb
1.39 𝜎= = = 𝟓𝟑𝟕𝟓 𝐩𝐬𝐢
𝐴 (0.40 in)2
𝑃 1850 lb = 𝟏𝟔 𝟕𝟓𝟎 𝐩𝐬𝐢
1.40 𝜎= =
𝐴 [(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
∑ 𝑀 = 0 = (9025 N)(600 mm) − 𝐶𝑉(1200 mm)
𝐶 = 4512 N

𝐶 = 𝐶𝑉/ sin 30° = 9025 N
𝐶 9025 N = 𝟕𝟗. 𝟖 𝐌𝐏𝐚
𝜎= = =
𝐴 𝐴 [(12 mm)2]⁄4
𝑃 70000 lb = 𝟏𝟑𝟗𝟑 𝐩𝐬𝐢
1.42 𝜎= =
𝐴 [(8 in)2]/4


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, (29500 lb)/3
1.43 𝜎= = = 𝟖𝟎𝟑 𝐩𝐬𝐢
𝐴 (3.5 in)2
𝑃 3500 N
1.44 𝜎= = = 𝟓𝟒. 𝟕 𝐌𝐏𝐚
𝐴 (8.0 mm)2
1.45 𝑊 = 𝑚 𝑔 = 4200 kg ∙ 9.81 m/s2 = 41.2 kN
𝐴𝐵 = 𝐴𝐵 sin 35°
𝐴𝐵 = 𝐴𝐵 cos 35°
𝐵𝐶 = 𝐵𝐶 sin 55°
𝐵𝐶 = 𝐵𝐶 cos 55°
∑ 𝐹 = 0 = 𝐴𝐵𝑋 − 𝐵𝐶𝑋
0 = 𝐴𝐵 sin 35° − 𝐵𝐶 sin 55°
sin 55°

𝐴𝐵 = 𝐵𝐶 ∙ sin 35° = 1.428 𝐵𝐶
∑ 𝐹 = 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 = 𝐵[1.170 + 0.574] = 1.743 𝐵𝐶
41.2 kN
𝐵𝐶 = = 23.63 kN
1.743

𝐴𝐵 = 1.428 𝐵𝐶 = 33.75 kN
𝐴𝐵 = 33.75×103 N = 𝟏𝟎𝟕. 𝟒 𝐌𝐏𝐚
Stress in Rod AB: 𝜎𝐴 = 𝐴 [(20 mm)2]/4
𝐵𝐶 = 23.63×103 N = 𝟕𝟓. 𝟐 𝐌𝐏𝐚
Stress in Rod BC: 𝜎𝐵 = 𝐴 [(20 mm)2]/4
𝐵𝐷 = 41.2×103 N = 𝟏𝟑𝟏. 𝟏 𝐌𝐏𝐚
Stress in Rod BD: 𝜎𝐵 = 𝐴 2
[(20 mm) ]/4
1.46 𝐹 = 0.01097 𝑚 𝑅 𝑛 =2 (0.01097)(0.40)(0.60)(3000)2
N

𝐹 = 23 695 N
(16 mm) 2
𝐴=
4 = 201 mm2
𝐹 23695 N = 𝟏𝟏𝟖 𝐌𝐏𝐚
𝜎= =
𝐴 201 mm2




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,1.47 𝐴 = (30 mm)2 = 900 mm2

For AB: 𝐹𝐴 = (110 − 40 + 80) 3kN = 150 kN
150×10 N
𝐹𝐴𝐵
=
𝜎𝐴𝐵 = 𝐴 900 mm2
= 𝟏𝟔𝟕 𝐌𝐏𝐚 Tension
For BC: 𝐹𝐵 = 110 − 40 = 70 3kN
𝐹𝐵𝐶
= 70×10 N = 𝟕𝟕. 𝟖 𝐌𝐏𝐚 Tension
𝜎𝐵𝐶 = 𝐴 900 mm2

For CD: 𝐹𝐶 = 110 kN 110×103 N
𝐹𝐶𝐷
=
𝜎𝐶𝐷 = 𝐴 900 mm2
= 𝟏𝟐𝟐 𝐌𝐏𝐚 Tension
1.48 Areas: A-C; 𝐴1 = 𝜋(25)2/4 = 491 mm2
C-D; 𝐴2 = 𝜋(16)2/4 = 201 mm2

For AB: 𝐹𝐴 = −9.65 − 12.32 + 4.45 = −17.52 kN
−17.52×103 N
𝐹𝐴𝐵

𝜎𝐴𝐵 = 𝐴1 = 491 mm2
= −𝟑𝟓. 𝟕 𝐌𝐏𝐚 Compression
For BC: 𝐹𝐵 = −9.65 − 12.32 = −21.97 kN
−21.97×103 N
𝐹𝐵𝐶

𝜎𝐵𝐶 = 𝐴1 = 491 mm2
= −𝟒𝟒. 𝟕 𝐌𝐏𝐚 Compression
For CD: 𝐹𝐶 = −9.65 kN −9.65×103 N
𝐹𝐶𝐷
𝜎𝐶𝐷 =
2
𝐴2
2
= 201 mm2
= −𝟒𝟖. 𝟎 𝐌𝐏𝐚 Compression
[(1.90) −(1.61) ] 1
1.49 𝐴= = 0.799 in2 [1 in Pipe-Appendix A-9(a)]
4 2
𝐹𝐵𝐶
= 2500 lb
= 𝟑𝟏𝟐𝟗 𝐩𝐬𝐢 Tension
For BC: 𝜎𝐵 = 𝐴 0.799 in2

For AB: 𝐹𝐴 = 2500 + 2(8000 cos 30°) = 16 356 lb
𝐹𝐴𝐵
= 16 356 lb = 𝟐𝟎 𝟒𝟕𝟏 𝐩𝐬𝐢 Tension
𝜎𝐴𝐵 = 𝐴 0.799 in2
1.50 ∑ 𝑀 = 0 = 2800(45) − 𝐹𝐵𝐷(30)

𝐹𝐵 = 4200 lb
𝐹𝐵𝐷
= 4200 lb = 𝟑𝟐𝟑𝟏 𝐩𝐬𝐢 Tension

𝜎𝐵𝐷 = 𝐴 (2.0)(0.65) in2




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,1.51 𝐴𝐷 sin 30° = 5.25 kN
𝐴𝐷 = 10.5 kN = 𝐶𝐷
𝐴𝐵 = 𝐴𝐷 cos 30° = 9.09 kN = 𝐵𝐶

Stresses:
9.09×103 N
𝐴𝐵, 𝐵𝐶: 𝜎 =𝜎 = = 𝟐𝟓. 𝟑 𝐌𝐏𝐚 Tension
𝐴𝐵 𝐵𝐶 (12)(30) mm 2
10.5×103 N
𝐵𝐷: 𝜎 = = 𝟏𝟕. 𝟓 𝐌𝐏𝐚 Tension
𝐵𝐷 (2)(10)(30) mm 2

𝐴𝐷, 𝐶𝐷: 𝐴 = (30)2 − (20)2 = 500 mm2
−10.5×103 N

𝜎𝐴𝐷 = 𝜎𝐶𝐷 = 500 mm2 = −𝟐𝟏. 𝟎 𝐌𝐏𝐚 Compression
1.52 ∑ 𝑀 = 0 = 6000(6) + 12 000(12) − 𝑅𝐹(18)
𝑅 = 10 000 lb
∑ 𝑀 = 0 = 12 000(6) + 6000(12) − 𝑅𝐴(18)


𝑅 = 8000 lb



𝑅 = 𝐴𝐵 sin 𝜃 = 𝐴𝐵(0.8)
𝑅 8000
𝐴𝐵 = = = 10 000 lb Compression
0.8 0.8




𝐴𝐷 = 𝐴𝐵 cos 𝜃 = 10 000(0.6) = 6000 lb Tension


𝐵𝐸 sin 𝜃 + 6000 − 𝐴𝐵 sin 𝜃 = 0
𝐴𝐵 sin 𝜃−6000 10 000(0.8)−6000
𝐵𝐸 = = = 2500 lb Tension
sin 𝜃 0.8
𝐵𝐶 = 𝐴𝐵 cos 𝜃 + 𝐵𝐸 cos 𝜃 = 10 000(0.6) + 2500(0.6)
[Continued on next page]




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, 𝐵𝐶 = 7500 lb Compression

𝐵𝐶 = 𝐶𝐹
𝐵𝐶
cos 𝜃7500
𝐶𝐹 = = = 12 500 lb Compression
cos 𝜃 0.6
𝐶𝐸 = 12 000 − 𝐶𝐹 sin 𝜃 = 12 000 − 12 500(0.8)
CE = 2000 lb Compression
EF = CF cos
members: = 12 500A-5(a)
Appendixes lb(0.6)and
= 7500 lb Tension Areas of
A-6(a)
AD, DE, EF – 2(0.484 in2) = 0.968 in2

BD, BE, CE – 0.484 in2
AB, BC, CF – 2(1.21 in2) = 2.42 in2
Stresses:
AD = DE = 6000/0.968 = +6198 psi

EF = 7500/0.968 = +7748 psi

BD = 0

BE = 2500/0.484 = +5165 psi

CE = -2000/0.484 = -4132 psi [NOTE: Compression members must be
AB = -10 000/2.42 = -4132 psi checked for column buckling.]
BC = -7500/2.42 = -3099 psi
CF = -12 500/2.42 = -5165 psi


1.53 𝐴𝐵 ∑= 𝑀
20 =kN03 = (12.5)(4.0) − 𝐴𝐵(2.5)
20×10 N = 𝟓𝟎 𝐌𝐏𝐚
𝜎= 2 2
(20) mm2
(0.505)
1.54 𝐴= = 0.200 in2
4
12 600 lb
𝜎= = = 𝟔𝟑 𝟎𝟎𝟎 𝐩𝐬𝐢
𝐴 0.200 in2

1.55 𝐴 = (2.65)(1.40) + 2[(1.40)(0.5)(𝑡)] = 4.41 in2
52 000 lb
𝜎= = = 𝟏𝟏 𝟕𝟗𝟏 𝐩𝐬𝐢
𝐴 4.41 in2 𝜋(40)2
1.56 𝐴 = (80)(40) − (60)(15) + = 3557 mm2
4
N
640×10
3
= 𝟏𝟖𝟎 𝐌𝐏𝐚
𝜎= =
𝐴 3557 mm2




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,1.57 Direct Shear – Single Shear
(12.0)2
] mm 2 2

𝐴𝑆 = [ 4
3
= 113 mm
𝐹 N
𝜏= 16.5×10 = 𝟏𝟒𝟔 𝐌𝐏𝐚
=
𝐴𝑆 113 mm2
1.58 ∑ 𝐹 = 0 = 55(145) − 𝐹𝑃 (45) Pin is in single
shear
𝐹 = 177 N
(3.0)2
= 7.07 mm 2

𝐴𝑆 = 4
𝐹 177 N = 𝟐𝟓. 𝟏 𝐌𝐏𝐚
𝜏= =
𝐴𝑆 7.07 mm2

1.59 From Problem
(10)2
1-46: 𝐹 = 23 695 N
] = 157 mm2 4
𝐴 = 2𝐹[ 23 695 N Double Shear
𝜏= = = 𝟏𝟓𝟏 𝐌𝐏𝐚
𝐴𝑆 157 mm2

1.60 𝐴 = (3.0)(3.5)
𝐹 1800 lb= 10.5 in
2
𝜏= = = 𝟏𝟕𝟏 𝐩𝐬𝐢
𝐴𝑆 10.5 in2

1.61 𝐴 = [2(35) + 𝜋(8)](50) = 475.7 mm2
3
𝐹 N
𝜏= 38.6×10 = 𝟖𝟏. 𝟏 𝐌𝐏𝐚
=
𝐴𝑆 475.7 mm2
1.62 𝐿 = √0.42 + 0.62 = 0.721 in
(0.8)
+ 2(0.721)] 0.194
𝐴 = [2(1.60) +
2
𝐴 = 1.144
𝐹
in2
45 000 lb
𝜏= = = 𝟑𝟗 𝟑𝟐𝟒 𝐩𝐬𝐢
𝐴𝑆 1.144 in2

1.63 𝑇 = 𝐹𝑆 ∙ 𝑅
95 N∙m 103 mm
𝑇
= 5429 N
𝐹= 𝑅
= 35 mm/2
∙
m

𝐴 = 𝑏 ∙ 𝐿 = (10)(22) = 220 mm2
𝐹 5429 N = 𝟐𝟒. 𝟕 𝐌𝐏𝐚
𝜏= =
𝐴𝑆 220 mm2




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, 𝑇
1.64 = = 8000 lb∙in
𝑆
= 8000 lb
𝑅 1.0 in

𝐴 = 𝑏 ∙ 𝐿 = (0.50)(2.25) = 1.125 in2
𝐹 8000 lb = 𝟕𝟏𝟏𝟏 𝐩𝐬𝐢
𝜏= =
𝐴𝑆 1.125 in2


1.65 Pin: Double
𝐹
Shear; 𝐴 = 2[𝜋(0.5)2/4] = 0.393 in2
20 000 lb
𝜏= = = 𝟓𝟎 𝟗𝟑𝟎 𝐩𝐬𝐢
𝐴𝑆 0.393 in2
Collar: Shear Collar from Connector Body

𝐴 = 𝜋𝑑𝑡
𝐹
= 𝜋(0.875)(0.1875) = 0.5154 in2
𝜏 = = 20 000 lb
𝐴𝑆 0.5154 in2 = 𝟑𝟖 𝟖𝟎𝟎 𝐩𝐬𝐢
1.66 ∑ 𝑀 = 0 = 800(80) − 𝐵𝑉(8)

𝐵 = 8000𝐵lb
𝐵 = cos 20°𝑉
= 8513 lb
(0.375)2
] = 0.221 in2 4
𝐴 = 2𝐵[
𝜏= = 8513 lb

𝐴𝑆 0.221 in2 = 𝟑𝟖 𝟓𝟒𝟎 𝐩𝐬𝐢
1.67 𝐴 = (40)(12) = 480 mm2
3
𝐹 N
𝜏= 88×10 = 𝟏𝟖𝟑 𝐌𝐏𝐚
=
𝐴𝑆 480 mm2
1.68 𝐴 = (40)(120) = 4800 mm2
3
𝐹 N
𝜏= 88.2×10 = 𝟏𝟖. 𝟒 𝐌𝐏𝐚
=
𝐴𝑆 4800 mm2
1.69 𝐴 = 𝜋𝑑𝑡 = 𝜋(12)(8) = 301.6 mm2
3
𝐹 N
𝜏= 22.3×10 = 𝟕𝟑. 𝟗 𝐌𝐏𝐚
=
𝐴𝑆 301.6 mm2
1.70 𝐴 = 2[𝜋(12) /4] = 226.2 mm2 Two Rivets – Single Shear
2
3
𝐹 N
𝜏= 10.2×10 = 𝟒𝟓. 𝟏 𝐌𝐏𝐚
=
𝐴𝑆 226.2 mm2
1.71 𝐴 = 4[𝜋(12) /4] = 452.4 mm2 Two Rivets – Double Shear
2
3
𝐹 N
𝜏= 10.2×10 = 𝟐𝟐. 𝟓𝟓 𝐌𝐏𝐚
=
𝐴𝑆 452.4 mm2




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