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Fundamental Formulas for Exam 1 in CE 220

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Fundamental Formulas for Exam 1 in CE 220 – Mechanics of Solids
Average Normal Stress, 𝝈
𝑃
𝜎=
𝐴
𝑃 = internal normal force acting on the desired cross-section
𝐴 = area of the desired cross-section
Note that 𝑃 and 𝐴 must correspond to the same cross-section
Average Shear Stress, 𝝉
𝑉
𝜏=
𝐴
𝑉 = internal shear force acting on the desired cross-section
𝐴 = area of the desired cross-section
Note that 𝑉 and 𝐴 must correspond to the same cross-section
Average Bearing Stress, πˆπ’ƒ
𝑃
πœŽπ‘ =
𝐴𝑏
𝑃 = internal normal force acting on the desired cross-section where bearing occurs
𝐴𝑏 = area of the desired cross-section where bearing occurs
Note that 𝑃 and 𝐴𝑏 must correspond to the same cross-section
For a round pin or bolt in a round hole, the diameter of the pin or bolt is used as the width of the
bearing area when calculating the average bearing stress
Factor of Safety, F.S.
πœŽπ‘“π‘Žπ‘–π‘™
πœπ‘“π‘Žπ‘–π‘™
𝐹. 𝑆. =
,
𝐹. 𝑆. =
,
πœŽπ‘Žπ‘™π‘™π‘œπ‘€
πœπ‘Žπ‘™π‘™π‘œπ‘€
𝐹. 𝑆. =
π‘ƒπ‘“π‘Žπ‘–π‘™
,
π‘ƒπ‘Žπ‘™π‘™π‘œπ‘€
𝐹. 𝑆. =
π‘‰π‘“π‘Žπ‘–π‘™
π‘‰π‘Žπ‘™π‘™π‘œπ‘€
Average Normal Strain, 𝜺
𝐿𝑓 − 𝐿𝑖
πœ€=
𝐿𝑖
𝐿𝑓 = final length between two points after deformation
𝐿𝑖 = initial length between two points before deformation
Shear Strain, 𝜸
πœ‹
𝛾 = − πœƒ′
2
πœ‹
πœƒ′ = final angle between two line segments for which the initial angle was 2
Poisson’s Ratio
πœ€π‘™π‘Žπ‘‘
𝜈=−
πœ€π‘™π‘œπ‘›π‘”
πœ€π‘™π‘Žπ‘‘ = lateral strain (perpendicular to applied normal stress, 𝜎)
πœ€π‘™π‘œπ‘›π‘” = longitudinal strain (parallel to applied normal stress, 𝜎)
Hooke’s Law for Stress and Strain
For uniaxial normal strain
𝜎 = πΈπœ€
𝜎 = normal stress
𝐸 = Elastic modulus (Young’s Modulus), slope of the initial linear portion of the 𝜎 − πœ€ diagram
πœ€ = normal strain
For shear strain
𝜏 = 𝐺𝛾
𝜏 = shear stress
𝐺 = Shear modulus (Modulus of Rigidity), the slope of the initial linear portion of the 𝜏 − 𝛾
diagram
𝜏 = shear strain
Generalized Hooke’s Law for multiaxial stress
1
1
πœ€π‘₯ = [𝜎π‘₯ − 𝜈(πœŽπ‘¦ + πœŽπ‘§ )],
πœ€π‘¦ = [πœŽπ‘¦ − 𝜈(𝜎π‘₯ + πœŽπ‘§ )],
𝐸
𝐸
𝜏π‘₯𝑦
πœπ‘¦π‘§
𝜏π‘₯𝑧
𝛾π‘₯𝑦 =
,
𝛾𝑦𝑧 =
,
𝛾π‘₯𝑧 =
𝐺
𝐺
𝐺
πœ€π‘§ =
1
[𝜎 − 𝜈(𝜎π‘₯ + πœŽπ‘¦ )]
𝐸 𝑧
Change in Length of Axially Loaded Members
For homogeneous and prismatic members subjected to an constant internal axial force
𝑃⋅𝐿
𝛿=
𝐴⋅𝐸
𝑃 = internal normal force acting member
𝐿 = the length of the member
𝐴 = the cross-sectional area of the member
𝐸 = the elastic modulus of the material from which the member is made
For members made of discrete sections that are individually homogeneous, prismatic, and subjected
to an constant internal axial force
𝑛
𝑃𝑖 ⋅ 𝐿𝑖
𝑃1 ⋅ 𝐿1 𝑃2 ⋅ 𝐿2
𝑃𝑛 ⋅ 𝐿𝑛
𝛿 = ∑(
)=
+
+ β‹―+
𝐴𝑖 ⋅ 𝐸𝑖
𝐴1 ⋅ 𝐸1 𝐴2 ⋅ 𝐸2
𝐴𝑛 ⋅ 𝐸𝑛
𝑖=1
𝑃𝑖 = internal normal force acting discrete member i
𝐿 = the length of discrete member i
𝐴 = the cross-sectional area of discrete member i
𝐸 = the elastic modulus of the material from which discrete member i is made
For homogeneous members that are non-prismatic and/or have a varying internal axial force
𝐿
𝑃(π‘₯)
𝛿=∫
𝑑π‘₯
0 𝐴(π‘₯) ⋅ 𝐸
𝑃(π‘₯) = a function describing the distribution of internal axial force along the member
𝐴(π‘₯) = a function describing the cross-sectional area along the length of the member
𝐸 = the elastic modulus of the material from which the member is made
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