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Chapter 07

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Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
Chapter 7 Analysis of Stress and Strain
7.1 Introduction
1. Flexure and shear formula (𝜎𝜎 = −𝑀𝑀𝑀𝑀/𝐼𝐼 and 𝜏𝜏 = 𝑉𝑉𝑉𝑉/𝐼𝐼𝐼𝐼), torsion formula (𝜏𝜏 = 𝑇𝑇𝑇𝑇/𝐼𝐼𝑃𝑃 ),
etc. help determine the stresses on cross sections
2. However, larger stresses may occur on inclined sections
3. Example 1: Uniaxial stress (Section 2.6) – maximum shear at 45° and maximum
normal at cross sections
4. Example 2: Pure shear (Section 3.5) – maximum tensile and compressive stresses
occur on 45°
5. Generalization of these examples οƒ  need theories for “Plane Stress”
6. Transformation equations help determine the stresses in any general direction from
the given state of stress
7.2 Plane Stress
1. Stress element under “plane stress” condition,
e.g. in the π‘₯π‘₯π‘₯π‘₯ plane: only the π‘₯π‘₯ and 𝑦𝑦 faces
of the element are subjected to stresses, and
all stresses act parallel to the π‘₯π‘₯ and 𝑦𝑦 axis.
2. Normal stress (𝜎𝜎)
-
Subscript identifies the face on which the
-
stress acts, e.g. 𝜎𝜎π‘₯π‘₯ and πœŽπœŽπ‘¦π‘¦
For e__________, equal normal stresses
act on the opposite faces
-
Sign convention: ________ is positive
while ___________ is negative
3. Shear stress (𝜏𝜏)
-
Two subscripts: the first indicates the face,
and the second direction
-
Sign convention: positive for plus(face)plus(direction), and negative otherwise
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
-
Junho Song
junhosong@snu.ac.kr
The sign convention described above is
consistent with the shear stress pattern
discussed in Section 1.7 (derived from the
equilibrium equation)
-
Thus, 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = πœπœπ‘¦π‘¦π‘¦π‘¦
ο‚€ Stresses on Inclined Sections
1. To express the stresses acting on the inclined
π‘₯π‘₯1 𝑦𝑦1 element in terms of those on the π‘₯π‘₯π‘₯π‘₯
element, consider the e__________ of the forces on the wedge-shaped element
2. Equilibrium equation in π‘₯π‘₯1 direction:
𝜎𝜎π‘₯π‘₯1 𝐴𝐴0 sec πœƒπœƒ − 𝜎𝜎π‘₯π‘₯ 𝐴𝐴0 cos πœƒπœƒ − 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ 𝐴𝐴0 sin πœƒπœƒ − πœŽπœŽπ‘¦π‘¦ 𝐴𝐴0 tan πœƒπœƒ sin πœƒπœƒ − πœπœπ‘¦π‘¦π‘¦π‘¦ 𝐴𝐴0 tan πœƒπœƒ cos πœƒπœƒ = 0
3. Equilibrium equation in 𝑦𝑦1 direction:
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 𝐴𝐴0 sec πœƒπœƒ + 𝜎𝜎π‘₯π‘₯ 𝐴𝐴0 sin πœƒπœƒ − 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ 𝐴𝐴0 cos πœƒπœƒ − πœŽπœŽπ‘¦π‘¦ 𝐴𝐴0 tan πœƒπœƒ cos πœƒπœƒ + πœπœπ‘¦π‘¦π‘¦π‘¦ 𝐴𝐴0 tan πœƒπœƒ sin πœƒπœƒ = 0
4. Using the relationship 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = πœπœπ‘¦π‘¦π‘¦π‘¦ , and also simplifying and rearranging, we obtain
𝜎𝜎π‘₯π‘₯1 = 𝜎𝜎π‘₯π‘₯ cos2 πœƒπœƒ + πœŽπœŽπ‘¦π‘¦ sin2 πœƒπœƒ + 2𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin πœƒπœƒ cos πœƒπœƒ
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −�𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ οΏ½ sin πœƒπœƒ cos πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ (cos2 πœƒπœƒ − sin2 πœƒπœƒ)
5. For πœƒπœƒ = 0, 𝜎𝜎π‘₯π‘₯1 =
6. For πœƒπœƒ = 90°, 𝜎𝜎π‘₯π‘₯1 =
and 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 =
and 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 =
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
ο‚€ Transformation Equations for Plane Stress
1. Using the following trigonometric identities:
1
1
1
cos2 πœƒπœƒ = (1 + cos 2πœƒπœƒ), sin2 πœƒπœƒ = (1 − cos 2πœƒπœƒ), sin πœƒπœƒ cos πœƒπœƒ = sin 2πœƒπœƒ
2
2
2
2. The transformation equation is expressed in a more convenient form
𝜎𝜎π‘₯π‘₯1 =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
+
cos 2πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ
2
2
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
sin 2πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ cos 2πœƒπœƒ
2
οƒ  transformation equation for plane stress
3. Normal stress on the 𝑦𝑦1 face – can be obtained by substituting πœƒπœƒ + 90°
πœŽπœŽπ‘¦π‘¦1 =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
−
cos 2πœƒπœƒ − 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ
2
2
4. It is noted that
𝜎𝜎π‘₯π‘₯1 + πœŽπœŽπ‘¦π‘¦1 = 𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
ο‚€ Special Cases of Plane Stress
1. Uniaxial stress, i.e. πœŽπœŽπ‘¦π‘¦ = 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ =
𝜎𝜎π‘₯π‘₯1 =
𝜎𝜎π‘₯π‘₯
(1 + cos 2πœƒπœƒ)
2
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −
𝜎𝜎π‘₯π‘₯
(sin 2πœƒπœƒ)
2
2. Pure shear, i.e. 𝜎𝜎π‘₯π‘₯ = πœŽπœŽπ‘¦π‘¦ =
𝜎𝜎π‘₯π‘₯1 = 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ cos 2πœƒπœƒ
3. Biaxial stress, i.e. 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ =
𝜎𝜎π‘₯π‘₯1 =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
2
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −
+
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
2
2
sin 2πœƒπœƒ
cos 2πœƒπœƒ
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
ο‚€ Example 7-1: Internal pressure
results in longitudinal stress
𝜎𝜎π‘₯π‘₯ = 6,000 psi and
circumferential stress πœŽπœŽπ‘¦π‘¦ =
12,000 psi. Differential
settlement after an earthquake
οƒ  rotation at support B οƒ  shear stress 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = 2,500 psi. Find the stresses acting on the
element when rotated through angle πœƒπœƒ = 45 °
7.3 Principal Stresses and Maximum Shear Stresses
ο‚€ Principal Stresses
1. Principal stresses: maximum and
minimum stresses (οƒ  occurs at every 90°)
2. Setting the derivative to be zero, i.e.
π‘‘π‘‘πœŽπœŽπ‘₯π‘₯1
= −�𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ οΏ½ sin 2πœƒπœƒ + 2𝜏𝜏π‘₯π‘₯π‘₯π‘₯ cos 2πœƒπœƒ = 0
𝑑𝑑𝑑𝑑
from which we get the principal angle πœƒπœƒπ‘π‘
tan 2πœƒπœƒπ‘π‘ =
2𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
Note: the principal angles for minimum and
maximum stresses are perpendicular to
each other (why?)
3. Substituting πœƒπœƒπ‘π‘ into the transformation
formula via (οƒ )
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
2 ,
𝑅𝑅 = οΏ½οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
cos 2πœƒπœƒπ‘π‘ =
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
,
2𝑅𝑅
sin 2πœƒπœƒπ‘π‘ =
4. The larger of the two principal stresses, 𝜎𝜎1
𝜎𝜎1 = 𝜎𝜎π‘₯π‘₯1 οΏ½πœƒπœƒπ‘π‘ οΏ½ =
=
=
Junho Song
junhosong@snu.ac.kr
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝑅𝑅
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
+
cos 2πœƒπœƒπ‘π‘ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒπ‘π‘
2
2
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
+
οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ οΏ½ οΏ½
2
2
2𝑅𝑅
𝑅𝑅
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
2
+ οΏ½οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
2
5. The smaller of the principal stresses, 𝜎𝜎2 οƒ  From the property 𝜎𝜎1 + 𝜎𝜎2 =
𝜎𝜎2 = 𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ − 𝜎𝜎1
=
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
2
− οΏ½οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
2
6. A single formula for the principal stresses
𝜎𝜎1,2 =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
2
± οΏ½οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
2
ο‚€ Principal Angles
1. Principal angles πœƒπœƒπ‘π‘1 and πœƒπœƒπ‘π‘2 (corresponding to 𝜎𝜎1 and 𝜎𝜎2 , respectively) are roots
2𝜏𝜏π‘₯π‘₯π‘₯π‘₯
of the equation tan 2πœƒπœƒπ‘π‘ = 𝜎𝜎
πœƒπœƒπ‘π‘2
π‘₯π‘₯ −πœŽπœŽπ‘¦π‘¦
οƒ  Check the normal stresses to determine πœƒπœƒπ‘π‘1 and
2. Alternatively, πœƒπœƒπ‘π‘1 is the root that satisfies both cos 2πœƒπœƒπ‘π‘1 =
Then πœƒπœƒπ‘π‘2 is 90° larger or smaller than πœƒπœƒπ‘π‘1
𝜎𝜎π‘₯π‘₯ −πœŽπœŽπ‘¦π‘¦
2𝑅𝑅
and sin 2πœƒπœƒπ‘π‘1 =
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝑅𝑅
ο‚€ Shear Stresses on the Principal Planes
1. If we set 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = 0 for the transformation equation 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −
2𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝜏𝜏π‘₯π‘₯π‘₯π‘₯ cos 2πœƒπœƒ, we get the equation tan 2πœƒπœƒ = 𝜎𝜎
for having principal stresses
π‘₯π‘₯ −πœŽπœŽπ‘¦π‘¦
𝜎𝜎π‘₯π‘₯ −πœŽπœŽπ‘¦π‘¦
2
sin 2πœƒπœƒ +
, which is the same as the condition
2. “The shear stresses are zero on the principal planes”
.
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
ο‚€ Maximum Shear Stresses
1. Setting the derivative to be zero, i.e.
π‘‘π‘‘πœπœπ‘₯π‘₯1 𝑦𝑦1
= −�𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ οΏ½ cos 2πœƒπœƒ − 2𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ = 0
π‘‘π‘‘πœƒπœƒ
tan 2πœƒπœƒπ‘ π‘  = −
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
2𝜏𝜏π‘₯π‘₯π‘₯π‘₯
tan 2πœƒπœƒπ‘ π‘  = −
1
tan 2πœƒπœƒπ‘π‘
2. Relationship between πœƒπœƒπ‘ π‘  and πœƒπœƒπ‘π‘ :
3. Can show (See textbook for the derivation) πœƒπœƒπ‘ π‘  = πœƒπœƒπ‘π‘ ± 45°
4. Maximum shear stress
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
𝜎𝜎 − 𝜎𝜎2
2 = 1
𝜏𝜏max = ��
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
2
ο‚€ Example 7-3: The state of stress in the
beam web at element C is 𝜎𝜎π‘₯π‘₯ = 86 MPa,
πœŽπœŽπ‘¦π‘¦ = −28 MPa, and 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = −32 MPa. (a)
Determine the principal stresses and show
them on a sketch of a properly oriented
element; and (b) Determine the maximum shear stresses and show them on a sketch of
a properly oriented element.
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
7.4 Mohr’s Circle for Plane Stress
ο‚€ Equations of Mohr’s Circle
1. Recall the transformation equation
𝜎𝜎π‘₯π‘₯1 =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
+
cos 2πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ
2
2
→ 𝜎𝜎π‘₯π‘₯1 −
𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 = −
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
=
cos 2πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ sin 2πœƒπœƒ
2
2
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
sin 2πœƒπœƒ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ cos 2πœƒπœƒ
2
2. It can be shown that
�𝜎𝜎π‘₯π‘₯1 −
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ 2
οΏ½ + 𝜏𝜏π‘₯π‘₯21 𝑦𝑦1 =
2
3. Note from the previous note that
𝜎𝜎aver =
𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦
2
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦ 2
2
𝑅𝑅 = οΏ½οΏ½
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
2
4. Now the equation above becomes
2
�𝜎𝜎π‘₯π‘₯1 − 𝜎𝜎aver οΏ½ + 𝜏𝜏π‘₯π‘₯21 𝑦𝑦1 = 𝑅𝑅 2
5. In words, (𝜎𝜎π‘₯π‘₯1 , 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 ) is located on a circle whose center is (
is ____
,
) and the radius
ο‚€ Construction of Mohr’s Circle
1. What’s required: _____, _____ and _____
2. Sign conventions (consistent with the transformation
formula, etc.)
-
Positive shear stress: d________
-
Positive normal stress: to the r______
-
Positive rotation: c___________
3. Construction procedure
1) Draw a set of coordinate axes with 𝜎𝜎π‘₯π‘₯1 as abscissa and 𝜏𝜏π‘₯π‘₯1 𝑦𝑦1 as ordinate
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
2) Locate the center C, (
,
Junho Song
junhosong@snu.ac.kr
)
3) Locate point A representing the stress condition ( , ) shown in Figure (a), πœƒπœƒ =
4) Locate point B representing the stress condition on the 𝑦𝑦 face, i.e. (
,
), πœƒπœƒ =
5) Draw a line AB. This goes through C (why?), i.e. opposite ends of the diameter of
the circle
6) Using Point C as the center, draw Mohr’s circle through points A and B. The
radius is the length of the line segments AC and BC, which is 𝑅𝑅 =
𝜎𝜎π‘₯π‘₯ −πœŽπœŽπ‘¦π‘¦ 2
οΏ½οΏ½
2
2
οΏ½ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯
ο‚€ Stresses on an Inclined Element
1. Consider the new axes π‘₯π‘₯1 and 𝑦𝑦1 after rotation πœƒπœƒ
2. From the point A representing the original state (𝜎𝜎π‘₯π‘₯ , πœŽπœŽπ‘¦π‘¦ ), rotate by 2πœƒπœƒ
c__________wise to locate the point D representing the inclined element
3. The coordinates of D are the normal and shear stresses of the inclined element
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
4. Proof: available in the textbook
ο‚€ Principal Stresses
1. The points 𝑃𝑃1 and 𝑃𝑃2 on Mohr’s
circle represent m________ and
m_________ normal stresses,
respectively οƒ  principal stresses
2. Principal stresses:
𝜎𝜎1 = 𝑂𝑂𝑂𝑂 + 𝐢𝐢𝑃𝑃1 =
𝜎𝜎2 = 𝑂𝑂𝑂𝑂 − 𝐢𝐢𝑃𝑃2 =
+
2
−
2
3. The angle of rotation to achieve the principal planes = the angle between A and 𝑃𝑃1
(or 𝑃𝑃2 ) divided by _____
4. The angle πœƒπœƒπ‘π‘1 can be obtained from
cos 2πœƒπœƒπ‘π‘1 =
𝜎𝜎π‘₯π‘₯ − πœŽπœŽπ‘¦π‘¦
2𝑅𝑅
sin 2πœƒπœƒπ‘π‘1 =
5. From Mohr’s circle, it is clear that
πœƒπœƒπ‘π‘2 = πœƒπœƒπ‘π‘1 +
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝑅𝑅
°
ο‚€ Maximum Shear Stresses
1. The points 𝑆𝑆1 and 𝑆𝑆2 on Mohr’s
circle represent maximum positive
and negative shear stresses,
respectively.
2. The angle between these points and
𝑃𝑃1 and 𝑃𝑃2 (on Mohr’s circle) =
3. This confirms once again that the
angle between principal stress and
maximum shear stresses is
4. The normal stresses under
maximum shear stresses =
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
ο‚€ Example 7-4: At a point on the surface of a hydraulic ram
on a piece of construction equipment, the material is
subjected to biaxial stresses 𝜎𝜎π‘₯π‘₯ = 90 MPa and πœŽπœŽπ‘¦π‘¦ =
20 MPa. Using Mohr’s circle, determine the stresses
acting on an element inclined at an angle πœƒπœƒ = 30°.
Junho Song
junhosong@snu.ac.kr
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
ο‚€ Example 7-5: An element in plane stress on the surface
of an oil-drilling pump arm is subjected to stresses 𝜎𝜎π‘₯π‘₯ =
100 MPa, πœŽπœŽπ‘¦π‘¦ = 34 MPa, and 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = 28 MPa. Using
Mohr’s circle, determine (a) the stresses acting on an
element inclined at an angle πœƒπœƒ = 40°, (b) the principal
stresses, and (c) the maximum shear stresses.
Junho Song
junhosong@snu.ac.kr
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
ο‚€ Example 7-6: At a point on the surface of a metalworking lathe the stresses are 𝜎𝜎π‘₯π‘₯ = −50 MPa, πœŽπœŽπ‘¦π‘¦ =
10 MPa, and 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = −40 MPa. Using Mohr’s circle,
determine (a) the stresses acting on an element inclined
at an angle πœƒπœƒ = 45°, (b) the principal stresses, and (c)
the maximum shear stresses.
Junho Song
junhosong@snu.ac.kr
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
7.5 Hooke’s Law for Plane Stress
ο‚€ Hooke’s Law for Plane Stress
1. Conditions (in addition to being in “Plane Stress”)
1) Material properties uniform throughout the body
and in all directions (h__________ and
i_________)
2) The material is l______ e______, i.e. follows
Hooke’s law
2. “Resultant” strains
1
1
𝜈𝜈
�𝜎𝜎π‘₯π‘₯ − πœˆπœˆπœŽπœŽπ‘¦π‘¦ οΏ½ πœ€πœ€π‘¦π‘¦ = οΏ½πœŽπœŽπ‘¦π‘¦ − 𝜈𝜈𝜎𝜎π‘₯π‘₯ οΏ½ πœ€πœ€π‘§π‘§ = − �𝜎𝜎π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ οΏ½
𝐸𝐸
𝐸𝐸
𝐸𝐸
πœ€πœ€π‘₯π‘₯ =
3. Shear strain: 𝛾𝛾π‘₯π‘₯π‘₯π‘₯ =
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
𝐺𝐺
4. Solving the equations of resultant strains simultaneously for 𝜎𝜎π‘₯π‘₯ and πœŽπœŽπ‘¦π‘¦ , we can
obtain “Hooke’s law for plane stress” as
𝜎𝜎π‘₯π‘₯ =
πœŽπœŽπ‘¦π‘¦ =
𝐸𝐸
οΏ½πœ€πœ€ + πœˆπœˆπœ€πœ€π‘¦π‘¦ οΏ½
1 − 𝜈𝜈 2 π‘₯π‘₯
𝐸𝐸
οΏ½πœ€πœ€ + πœˆπœˆπœ€πœ€π‘₯π‘₯ οΏ½
1 − 𝜈𝜈 2 𝑦𝑦
𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = 𝐺𝐺𝛾𝛾π‘₯π‘₯π‘₯π‘₯
5. Hooke’s law for plane stress contain three material constants: 𝐸𝐸, 𝐺𝐺, and 𝜈𝜈, but only
two are independent because of the relationship
𝐺𝐺 =
𝐸𝐸
2(1 + 𝜈𝜈)
ο‚€ Volume Change (for Plane Stress)
1. Original volume: 𝑉𝑉0 = π‘Žπ‘Žπ‘Žπ‘Žπ‘Žπ‘Ž
2. Final volume: 𝑉𝑉1 = (π‘Žπ‘Ž + π‘Žπ‘Žπœ€πœ€π‘₯π‘₯ )�𝑏𝑏 + π‘π‘πœ€πœ€π‘¦π‘¦ οΏ½(𝑐𝑐 + π‘π‘πœ€πœ€π‘§π‘§ )
3. Volume change: π›₯π›₯π›₯π›₯ = 𝑉𝑉1 − 𝑉𝑉0 ≅ 𝑉𝑉0 (πœ€πœ€π‘₯π‘₯ + πœ€πœ€π‘¦π‘¦ + πœ€πœ€π‘§π‘§ )
4. Unit volume change (“dilatation”):
𝑒𝑒 = π›₯π›₯π›₯π›₯/𝑉𝑉0 =
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
ο‚€ Strain-Energy Density (for Plane Stress)
1. Work done by the force on π‘₯π‘₯-face and 𝑦𝑦-face:
1
1
(𝜎𝜎π‘₯π‘₯ 𝑏𝑏𝑏𝑏)(π‘Žπ‘Žπœ€πœ€π‘₯π‘₯ ) + οΏ½πœŽπœŽπ‘¦π‘¦ π‘Žπ‘Žπ‘Žπ‘ŽοΏ½οΏ½π‘π‘πœ€πœ€π‘¦π‘¦ οΏ½
2
2
π‘Žπ‘Žπ‘Žπ‘Žπ‘Žπ‘Ž
=
�𝜎𝜎π‘₯π‘₯ πœ€πœ€π‘₯π‘₯ + πœŽπœŽπ‘¦π‘¦ πœ€πœ€π‘¦π‘¦ οΏ½
2
2. Strain energy density by the normal stresses:
𝑒𝑒1 =
1
�𝜎𝜎 πœ€πœ€ + πœŽπœŽπ‘¦π‘¦ πœ€πœ€π‘¦π‘¦ οΏ½
2 π‘₯π‘₯ π‘₯π‘₯
𝑒𝑒2 =
𝜏𝜏π‘₯π‘₯π‘₯π‘₯ 𝛾𝛾π‘₯π‘₯π‘₯π‘₯
2
3. Strain energy density associated with the shear stresses:
4. Strain energy density in plane stress:
𝑒𝑒 =
1
�𝜎𝜎 πœ€πœ€ + πœŽπœŽπ‘¦π‘¦ πœ€πœ€π‘¦π‘¦ + 𝜏𝜏π‘₯π‘₯π‘₯π‘₯ 𝛾𝛾π‘₯π‘₯π‘₯π‘₯ οΏ½
2 π‘₯π‘₯ π‘₯π‘₯
𝑒𝑒 =
2
𝜏𝜏π‘₯π‘₯π‘₯π‘₯
1
�𝜎𝜎π‘₯π‘₯2 + πœŽπœŽπ‘¦π‘¦2 − 2𝜈𝜈𝜎𝜎π‘₯π‘₯ πœŽπœŽπ‘¦π‘¦ οΏ½ +
2𝐸𝐸
2𝐺𝐺
5. Using Hooke’s law, the strain energy density can be alternatively described as
𝑒𝑒 =
2
𝐺𝐺𝛾𝛾π‘₯π‘₯π‘₯π‘₯
𝐸𝐸
2
2
οΏ½πœ€πœ€
+
πœ€πœ€
+
2πœˆπœˆπœ€πœ€
πœ€πœ€
οΏ½
+
𝑦𝑦
π‘₯π‘₯ 𝑦𝑦
2
2(1 − 𝜈𝜈 2 ) π‘₯π‘₯
ο‚€ Example 7-7: Consider a rectangular plate
with thickness 𝑑𝑑 = 7mm under plane stress
(biaxial) condition. The readings of the gages
A and B give πœ€πœ€π‘₯π‘₯ = −0.00075 and πœ€πœ€π‘¦π‘¦ =
0.00125. 𝐸𝐸 = 73 GPa and ν = 0.33. Find the
stresses 𝜎𝜎π‘₯π‘₯ and πœŽπœŽπ‘¦π‘¦ and the change Δ𝑑𝑑 in
the thickness. Find the volume change (or
dilatation) 𝑒𝑒 and the strain energy density 𝑒𝑒 for the plate.
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
7.7 Plane Strain
ο‚€ Plane Strain Versus Plane Stress
1. Recall “plane stress” condition:
πœŽπœŽπ‘§π‘§ = 0
𝜏𝜏π‘₯π‘₯π‘₯π‘₯ = 0 πœπœπ‘¦π‘¦π‘¦π‘¦ = 0
2. “Plane strain” condition:
πœ€πœ€π‘§π‘§ = 0
𝛾𝛾π‘₯π‘₯π‘₯π‘₯ = 0
𝛾𝛾𝑦𝑦𝑦𝑦 = 0
Junho Song
junhosong@snu.ac.kr
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
3. Under ordinary conditions, plane stress and strain (do/do not) occur simultaneously.
4. The following exceptional cases of plane stress = plain strain (why?)
1) Plane stress with 𝜎𝜎π‘₯π‘₯ = −πœŽπœŽπ‘¦π‘¦
2) Zero Poisson effect, i.e. ν = 0
ο‚€ Transformation Equations for Plane Strain
1. Transformation equations (Proof in Textbook)
πœ€πœ€π‘₯π‘₯1 =
πœ€πœ€π‘₯π‘₯ + πœ€πœ€π‘¦π‘¦ πœ€πœ€π‘₯π‘₯ − πœ€πœ€π‘¦π‘¦
𝛾𝛾π‘₯π‘₯π‘₯π‘₯
+
cos 2πœƒπœƒ +
sin 2πœƒπœƒ
2
2
2
𝛾𝛾π‘₯π‘₯1 𝑦𝑦1
πœ€πœ€π‘₯π‘₯ − πœ€πœ€π‘¦π‘¦
𝛾𝛾π‘₯π‘₯π‘₯π‘₯
=−
sin 2πœƒπœƒ +
cos 2πœƒπœƒ
2
2
2
2. Sum of strains is conserved, i.e. πœ€πœ€π‘₯π‘₯ + πœ€πœ€π‘¦π‘¦ = const
3. Principal strains
tan 2πœƒπœƒπ‘π‘ =
πœ€πœ€1,2 =
𝛾𝛾π‘₯π‘₯π‘₯π‘₯
πœ€πœ€π‘₯π‘₯ − πœ€πœ€π‘¦π‘¦
πœ€πœ€π‘₯π‘₯ + πœ€πœ€π‘¦π‘¦
πœ€πœ€π‘₯π‘₯ − πœ€πœ€π‘¦π‘¦ 2
𝛾𝛾π‘₯π‘₯π‘₯π‘₯ 2
οΏ½ +οΏ½ οΏ½
± οΏ½οΏ½
2
2
2
4. Maximum shear strains and corresponding normal strains
πœ€πœ€π‘₯π‘₯ − πœ€πœ€π‘¦π‘¦ 2
𝛾𝛾π‘₯π‘₯π‘₯π‘₯ 2
𝛾𝛾max
οΏ½ +οΏ½ οΏ½
= οΏ½οΏ½
2
2
2
πœ€πœ€aver =
πœ€πœ€π‘₯π‘₯ + πœ€πœ€π‘¦π‘¦
2
5. Mohr’s circle for strains (οƒ )
6. Applications of transformation
equations: one can use
transformation equations for
plane strain for plane stress
conditions (and vice versa)
because πœ€πœ€π‘§π‘§ does not affect the
strains
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
Junho Song
junhosong@snu.ac.kr
ο‚€ Strain Measurements
1. Electrical-resistance strain gage measures n_________ strain in t______ directions
with 45° angle differences (why?)
2. How it works: electrical resistance of wire is altered when it stretches or shortens
ο‚€ Example 7-8: Consider a plane strain
condition with πœ€πœ€π‘₯π‘₯ = 340 × 10−6 , πœ€πœ€π‘¦π‘¦ = 110 ×
10−6 , 𝛾𝛾π‘₯π‘₯π‘₯π‘₯ = 180 × 10−6 . Determine (a)
strains at πœƒπœƒ = 30°, (b) principal strains, and
(c) maximum shear strains.
Dept. of Civil and Environmental Engineering, Seoul National University
457.201 Mechanics of Materials and Lab.
ο‚€ Example 7-9: Explain how to obtain strains πœ€πœ€π‘₯π‘₯1 , πœ€πœ€π‘¦π‘¦1
and 𝛾𝛾π‘₯π‘₯1 𝑦𝑦1 associated with an angle πœƒπœƒ from the
gage readings πœ€πœ€π‘Žπ‘Ž , πœ€πœ€π‘π‘ and πœ€πœ€π‘π‘ .
Junho Song
junhosong@snu.ac.kr
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