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1 
Copyright© 2001 
Content 
 Stress Transformation 
 A Mini Quiz 
 Strain Transformation 
CClliicckk hheerree 
CClliicckk hheerree 
CClliicckk hheerree 
Approximate Duration: 20 minutes
N. Sivakugan 
Copyright© 2001 
Plane Stress Transformation
3 
Copyright© 2001 
Plane Stress Loading 
x 
y 
~ where all elements of the body 
are subjected to normal and shear 
stresses acting along a plane (x-y); 
none perpendicular to the plane (z-direction) 
sz = 0; txz = 0; tzy = 0
4 
Copyright© 2001 
Plane Stress Loading 
x 
y 
Therefore, the state of stress at a 
point can be defined by the three 
independent stresses: 
sx; sy; and txy 
sx 
sy txy 
A 
A
5 
Copyright© 2001 
Objective 
A 
x 
y 
sx 
sy txy 
A 
State of Stress at A 
If sx, sy, and txy 
are known, …
6 
Copyright© 2001 
Objective 
A 
x 
y 
s’x 
s’y t’xy 
A 
State of Stress at A 
…what would be 
s’x, s’y, and t’xy? 
x’ 
y’ 
q
7 
Copyright© 2001 
Transformation 
x 
y 
x’ 
y’ 
q 
sy txy 
q sx 
A 
State of Stress at A 
txy 
s’x t’xy=? =?
8 
Copyright© 2001 
Transformation 
Solving equilibrium equations for the wedge… 
æ - 
+ ÷ ÷ø 
æ + 
= 
x + ÷ ÷ø 
q t q 
s s s s 
x y x y 
s cos 2 sin 2 
' xy 
2 2 
ö 
ç çè 
ö 
ç çè 
æ - 
x y 
' s c xy 
xy + ÷ ÷ø 
q t q 
s s 
t in 2 os 2 
2 
ö 
ç çè 
= -
9 
Copyright© 2001 
Principal Planes & Principal Stresses 
Principal 
Plan~ earse the two planes where the normal stress (s) is 
the maximum or minimum 
~ there are no shear stresses on principal planes 
~ these two planes are mutually perpendicular 
~ the orientations of the planes (qp) are given by: 
ö 
÷ ÷ø 
æ 
ç çè 
t 
xy 
1 1 
p s - 
s 
= - 
x y 
q 
2 
tan 
2 
gives two values (qp1 and qp2)
10 
Copyright© 2001 
Principal Planes & Principal 
Stresses 
x 
qp1 
Orientation of Principal 
Planes 
qp2 
90°
æ - 
s s 
ö 
R x y t 
+ ÷ ÷ø 
11 
Copyright© 2001 
Principal Planes & Principal Stresses 
Principal 
Stres~s aeres the normal stresses (s) acting on the principal planes 
ö 
æ + 
s s 
R y x + ÷ ÷ø 
ç çè 
s s 
= = 
max 1 2 
ö 
æ + 
s s 
R y x - ÷ ÷ø 
ç çè 
s s 
= = 
min 2 2 
2 
2 
2 xy 
ç çè 
=
12 
Copyright© 2001 
Maximum Shear (tmax) 
~ maximum shear stress occurs on two mutually 
perpendicular planes 
~ orientations of the two planes (qs) are given by: 
ö 
÷ ÷ø 
æ - 
ç çè 
1 1 
= - - 
s s 
x y 
s t 
xy 
q 
2 
tan 
2 
gives two values (qs1 and qs2) 
 tmax = R 
2 
2 
æ - 
s s 
ö 
R x y t 
+ ÷ ÷ø 
2 xy 
ç çè 
=
13 
Copyright© 2001 
Maximum Shear 
x 
Orientation of Maximum Shear Planes 
qs1 
qs2 
90°
14 
Copyright© 2001 
Principal Planes & Maximum Shear 
Planes 
x 
Principal plane 
Maximum shear plane 
qp = qs ± 
45° 
45°
15 
Copyright© 2001 
Mohr Circles 
From the stress-transformation equations (slide 7), 
2 2 
2 
æ + 
- x y 
ö 
t 
' R xy 
x 2 
úû 
+ ' 
= ù 
é 
êë 
÷ ÷ø 
ç çè 
s s 
s 
Equation of a circle, with 
variables being sx’ and txy’
16 
Copyright© 2001 
Mohr Circles 
sx’ 
txy’ 
(sx + sy)/2 
R
17 
Copyright© 2001 
Mohr Circles 
A point on the Mohr circle represents the sx’ 
and txy’ values on a specific plane. 
 q is measured counterclockwise from the 
original x-axis. 
Same sign convention for stresses as before. 
i.e., on positive planes, pointing positive directions 
positive, and ….
18 
Copyright© 2001 
Mohr Circles 
sx’ 
txy’ 
q = 90° 
q = 0 
q 
When we rotate the 
plane by 180°, we go a 
full round (i.e., 360°, 
on the Mohr circle. 
Therefore….
19 
Copyright© 2001 
Mohr Circles 
sx’ 
txy’ 
q 
…..when we rotate the 
plane by q°, we go 2q° 
on the Mohr circle. 
2q
20 
Copyright© 2001 
Mohr Circles 
sx’ 
txy’ 
s2 
s1 
tmax
21 
Copyright© 2001 
From the three Musketeers 
Get the sign 
convention right 
Mohr circle is a 
simple but powerful 
technique 
Mohr circle represents the 
state of stress at a point; thus 
different Mohr circles for 
different points in the body 
QQuuiitt CCoonnttiinnuuee
200 kPa 
60 kPa 
22 
Copyright© 2001 
A Mohr Circle Problem 
A 40 kPa 
The stresses at a point A are 
shown on right. 
Find the following: 
 major and minor principal stresses, 
 orientations of principal planes, 
 maximum shear stress, and 
 orientations of maximum shear stress planes.
200 kPa 
60 kPa 
A 40 kPa 
s (kPa) 
Drawing Mohr Circle 
t (kPa) 
R = 100 
120
s (kPa) 
Principal Stresses 
t (kPa) 
s1= 220 
s2= 20 
R = 100
s (kPa) 
t (kPa) 
tmax = 100 
Maximum Shear Stresses
200 kPa 
60 kPa 
A 40 kPa 
s (kPa) 
Positions of x & y Planes 
on Mohr Circle 
t (kPa) 
R = 100 
120 
60 
40 
60 
q 
tan q = 60/80 
q = 36.87°
200 kPa 
60 kPa 
s (kPa) 
Orientations of Principal Planes 
t (kPa) 
A 40 kPa 
36.9° 
18.4° 
major principal 
plane 
minor principal 
plane 
71.6°
Orientations of Max. Shear 
Stress Planes 
200 kPa 
60 kPa 
s (kPa) 
t (kPa) 
A 40 kPa 
53.1° 
26.6° 
36.9° 
116.6°
29 
Copyright© 2001 
Testing Times… 
Do you want to try a mini quiz? 
YYEESS Oh, NO!
Question 1: 
90 kPa 
The state of stress at a point A 40 kPa 
is shown. 
What would be the maximum 
shear stress at this point? 
A 30 kPa 
Answer 1: 50 kPa 
Press RETURN for the answer Press RETURN to continue
Question 2: 
90 kPa 
40 kPa At A, what would be the 
principal stresses? 
A 30 kPa 
Answer 2: 10 kPa, 110 kPa 
Press RETURN for the answer Press RETURN to continue
Question 3: 
90 kPa 
40 kPa At A, will there be any 
compressive stresses? 
A 30 kPa 
Answer 3: No. The minimum normal stress is 10 kPa (tensile). 
Press RETURN for the answer Press RETURN to continue
Question 4: 
90 kPa 
The state of stress at a point B 0 kPa 
is shown. 
What would be the maximum 
shear stress at this point? 
B 90 kPa 
Answer 4: 0 
This is hydrostatic state of 
stress (same in all directions). 
No shear stresses. 
Press RETURN for the answer Press RETURN to continue
N. Sivakugan 
Copyright© 2001 
Plane Strain Transformation
35 
Copyright© 2001 
Plane Strain Loading 
x 
y 
~ where all elements of the body 
are subjected to normal and shear 
strains acting along a plane (x-y); 
none perpendicular to the plane (z-direction) 
ez = 0; gxz = 0; gzy = 0
36 
Copyright© 2001 
Plane Strain Transformation 
Similar to previous derivations. Just replace 
s by e, and 
t by g/2
37 
Copyright© 2001 
Plane Strain Transformation 
Sign Convention: 
Normal strains (ex and ey): extension positive 
Shear strain (g ): decreasing angle positive 
e.g., 
x 
y 
before 
x 
y 
after 
ex positive 
ey negative 
g positive
38 
Copyright© 2001 
Plane Strain Transformation 
q 
g 
æ - 
+ ÷ ÷ø 
æ + 
= 
' x y x y q 
x ÷ø 
xy 
÷ + e e e e 
e sin 2 
2 
cos 2 
2 2 
ö 
ç çè 
ö 
ç çè 
q 
g 
æ - 
xy x y s q 
+ xy c ÷ø 
÷ g e e 
os 2 
2 
in 2 
' 
2 2 
ö 
ç çè 
= - 
Same format as the stress 
transformation equations
~ maximum (e1) and minimum (e2) principal strains 
~ occur along two mutually perpendicular directions, given by: 
R = x y xy 
39 
Copyright© 2001 
Principal Strains 
ö 
÷ ÷ø 
æ 
ç çè 
g 
xy 
1 
p e - 
e 
= - 
x y 
q tan 1 
2 
Gives two values (qp1 and qp2) 
ö 
ç çè æ + 
e e 
R y x + ÷ ÷ø 
e 
= 
1 2 
ö 
æ + 
= 
1 2 
R y x - ÷ ÷ø 
ç çè 
e e 
e 
2 2 
ö 
+ æ ÷ ÷ø 
æ - 
2 2 ÷ ÷ø 
ç çè 
ö 
ç çè 
e e g
40 
Copyright© 2001 
Maximum Shear Strain (gmax) 
gmax/2 = R 
2 2 
ö 
+ æ ÷ ÷ø 
æ - 
R = x y xy 
2 2 ÷ ÷ø 
ç çè 
ö 
ç çè 
e e g 
qp = qs ± 
45°
41 
Copyright© 2001 
Mohr Circles 
(ex + ey)/2 
R ex’ 
gxy’ 
2
42 
Copyright© 2001 
Strain Gauge 
~ measures normal strain (e), from the change in 
electrical resistance during deformation 
electrical resistance 
strain gauge
43 
Copyright© 2001 
Strain Rosettes 
~ measure normal strain (e) in three directions; use 
these to find ex, ey, and gxy 
e.g., 45° Strain Rosette 
x 
e90 
45° e0 
45° 
e45 
ex = e0 
measured 
ey = e90 
gxy = 2 e45 – (e0 + e90)
Mohr circle (Complete Soil Mech. Undestanding Pakage: ABHAY)

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Mohr circle (Complete Soil Mech. Undestanding Pakage: ABHAY)

  • 1. 1 Copyright© 2001 Content  Stress Transformation  A Mini Quiz  Strain Transformation CClliicckk hheerree CClliicckk hheerree CClliicckk hheerree Approximate Duration: 20 minutes
  • 2. N. Sivakugan Copyright© 2001 Plane Stress Transformation
  • 3. 3 Copyright© 2001 Plane Stress Loading x y ~ where all elements of the body are subjected to normal and shear stresses acting along a plane (x-y); none perpendicular to the plane (z-direction) sz = 0; txz = 0; tzy = 0
  • 4. 4 Copyright© 2001 Plane Stress Loading x y Therefore, the state of stress at a point can be defined by the three independent stresses: sx; sy; and txy sx sy txy A A
  • 5. 5 Copyright© 2001 Objective A x y sx sy txy A State of Stress at A If sx, sy, and txy are known, …
  • 6. 6 Copyright© 2001 Objective A x y s’x s’y t’xy A State of Stress at A …what would be s’x, s’y, and t’xy? x’ y’ q
  • 7. 7 Copyright© 2001 Transformation x y x’ y’ q sy txy q sx A State of Stress at A txy s’x t’xy=? =?
  • 8. 8 Copyright© 2001 Transformation Solving equilibrium equations for the wedge… æ - + ÷ ÷ø æ + = x + ÷ ÷ø q t q s s s s x y x y s cos 2 sin 2 ' xy 2 2 ö ç çè ö ç çè æ - x y ' s c xy xy + ÷ ÷ø q t q s s t in 2 os 2 2 ö ç çè = -
  • 9. 9 Copyright© 2001 Principal Planes & Principal Stresses Principal Plan~ earse the two planes where the normal stress (s) is the maximum or minimum ~ there are no shear stresses on principal planes ~ these two planes are mutually perpendicular ~ the orientations of the planes (qp) are given by: ö ÷ ÷ø æ ç çè t xy 1 1 p s - s = - x y q 2 tan 2 gives two values (qp1 and qp2)
  • 10. 10 Copyright© 2001 Principal Planes & Principal Stresses x qp1 Orientation of Principal Planes qp2 90°
  • 11. æ - s s ö R x y t + ÷ ÷ø 11 Copyright© 2001 Principal Planes & Principal Stresses Principal Stres~s aeres the normal stresses (s) acting on the principal planes ö æ + s s R y x + ÷ ÷ø ç çè s s = = max 1 2 ö æ + s s R y x - ÷ ÷ø ç çè s s = = min 2 2 2 2 2 xy ç çè =
  • 12. 12 Copyright© 2001 Maximum Shear (tmax) ~ maximum shear stress occurs on two mutually perpendicular planes ~ orientations of the two planes (qs) are given by: ö ÷ ÷ø æ - ç çè 1 1 = - - s s x y s t xy q 2 tan 2 gives two values (qs1 and qs2) tmax = R 2 2 æ - s s ö R x y t + ÷ ÷ø 2 xy ç çè =
  • 13. 13 Copyright© 2001 Maximum Shear x Orientation of Maximum Shear Planes qs1 qs2 90°
  • 14. 14 Copyright© 2001 Principal Planes & Maximum Shear Planes x Principal plane Maximum shear plane qp = qs ± 45° 45°
  • 15. 15 Copyright© 2001 Mohr Circles From the stress-transformation equations (slide 7), 2 2 2 æ + - x y ö t ' R xy x 2 úû + ' = ù é êë ÷ ÷ø ç çè s s s Equation of a circle, with variables being sx’ and txy’
  • 16. 16 Copyright© 2001 Mohr Circles sx’ txy’ (sx + sy)/2 R
  • 17. 17 Copyright© 2001 Mohr Circles A point on the Mohr circle represents the sx’ and txy’ values on a specific plane.  q is measured counterclockwise from the original x-axis. Same sign convention for stresses as before. i.e., on positive planes, pointing positive directions positive, and ….
  • 18. 18 Copyright© 2001 Mohr Circles sx’ txy’ q = 90° q = 0 q When we rotate the plane by 180°, we go a full round (i.e., 360°, on the Mohr circle. Therefore….
  • 19. 19 Copyright© 2001 Mohr Circles sx’ txy’ q …..when we rotate the plane by q°, we go 2q° on the Mohr circle. 2q
  • 20. 20 Copyright© 2001 Mohr Circles sx’ txy’ s2 s1 tmax
  • 21. 21 Copyright© 2001 From the three Musketeers Get the sign convention right Mohr circle is a simple but powerful technique Mohr circle represents the state of stress at a point; thus different Mohr circles for different points in the body QQuuiitt CCoonnttiinnuuee
  • 22. 200 kPa 60 kPa 22 Copyright© 2001 A Mohr Circle Problem A 40 kPa The stresses at a point A are shown on right. Find the following:  major and minor principal stresses,  orientations of principal planes,  maximum shear stress, and  orientations of maximum shear stress planes.
  • 23. 200 kPa 60 kPa A 40 kPa s (kPa) Drawing Mohr Circle t (kPa) R = 100 120
  • 24. s (kPa) Principal Stresses t (kPa) s1= 220 s2= 20 R = 100
  • 25. s (kPa) t (kPa) tmax = 100 Maximum Shear Stresses
  • 26. 200 kPa 60 kPa A 40 kPa s (kPa) Positions of x & y Planes on Mohr Circle t (kPa) R = 100 120 60 40 60 q tan q = 60/80 q = 36.87°
  • 27. 200 kPa 60 kPa s (kPa) Orientations of Principal Planes t (kPa) A 40 kPa 36.9° 18.4° major principal plane minor principal plane 71.6°
  • 28. Orientations of Max. Shear Stress Planes 200 kPa 60 kPa s (kPa) t (kPa) A 40 kPa 53.1° 26.6° 36.9° 116.6°
  • 29. 29 Copyright© 2001 Testing Times… Do you want to try a mini quiz? YYEESS Oh, NO!
  • 30. Question 1: 90 kPa The state of stress at a point A 40 kPa is shown. What would be the maximum shear stress at this point? A 30 kPa Answer 1: 50 kPa Press RETURN for the answer Press RETURN to continue
  • 31. Question 2: 90 kPa 40 kPa At A, what would be the principal stresses? A 30 kPa Answer 2: 10 kPa, 110 kPa Press RETURN for the answer Press RETURN to continue
  • 32. Question 3: 90 kPa 40 kPa At A, will there be any compressive stresses? A 30 kPa Answer 3: No. The minimum normal stress is 10 kPa (tensile). Press RETURN for the answer Press RETURN to continue
  • 33. Question 4: 90 kPa The state of stress at a point B 0 kPa is shown. What would be the maximum shear stress at this point? B 90 kPa Answer 4: 0 This is hydrostatic state of stress (same in all directions). No shear stresses. Press RETURN for the answer Press RETURN to continue
  • 34. N. Sivakugan Copyright© 2001 Plane Strain Transformation
  • 35. 35 Copyright© 2001 Plane Strain Loading x y ~ where all elements of the body are subjected to normal and shear strains acting along a plane (x-y); none perpendicular to the plane (z-direction) ez = 0; gxz = 0; gzy = 0
  • 36. 36 Copyright© 2001 Plane Strain Transformation Similar to previous derivations. Just replace s by e, and t by g/2
  • 37. 37 Copyright© 2001 Plane Strain Transformation Sign Convention: Normal strains (ex and ey): extension positive Shear strain (g ): decreasing angle positive e.g., x y before x y after ex positive ey negative g positive
  • 38. 38 Copyright© 2001 Plane Strain Transformation q g æ - + ÷ ÷ø æ + = ' x y x y q x ÷ø xy ÷ + e e e e e sin 2 2 cos 2 2 2 ö ç çè ö ç çè q g æ - xy x y s q + xy c ÷ø ÷ g e e os 2 2 in 2 ' 2 2 ö ç çè = - Same format as the stress transformation equations
  • 39. ~ maximum (e1) and minimum (e2) principal strains ~ occur along two mutually perpendicular directions, given by: R = x y xy 39 Copyright© 2001 Principal Strains ö ÷ ÷ø æ ç çè g xy 1 p e - e = - x y q tan 1 2 Gives two values (qp1 and qp2) ö ç çè æ + e e R y x + ÷ ÷ø e = 1 2 ö æ + = 1 2 R y x - ÷ ÷ø ç çè e e e 2 2 ö + æ ÷ ÷ø æ - 2 2 ÷ ÷ø ç çè ö ç çè e e g
  • 40. 40 Copyright© 2001 Maximum Shear Strain (gmax) gmax/2 = R 2 2 ö + æ ÷ ÷ø æ - R = x y xy 2 2 ÷ ÷ø ç çè ö ç çè e e g qp = qs ± 45°
  • 41. 41 Copyright© 2001 Mohr Circles (ex + ey)/2 R ex’ gxy’ 2
  • 42. 42 Copyright© 2001 Strain Gauge ~ measures normal strain (e), from the change in electrical resistance during deformation electrical resistance strain gauge
  • 43. 43 Copyright© 2001 Strain Rosettes ~ measure normal strain (e) in three directions; use these to find ex, ey, and gxy e.g., 45° Strain Rosette x e90 45° e0 45° e45 ex = e0 measured ey = e90 gxy = 2 e45 – (e0 + e90)