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Top School in Delhi NCR 
:By 
school.edhole.com
2 
Section IV 
Failures Due to Static 
Loading 
school.edhole.com
3 
Talking Points 
 Static Loading? 
 Failure Theories: 
 Maximum-Normal Stress Theory 
 Maximum-Shear Stress Theory 
 The Distortion-Energy Theory 
 Factor of Safety for each Failure 
Theory 
school.edhole.com
4 
?Static Loading 
 Static Load is a stationary force or moment 
acting on a member. 
 Stationary means that the force or moment 
does not change in magnitude. 
 Sometime the load is assumed to be static 
when it is known that some variation to be 
expected. Such assumptions are made to 
simplify the design computations when 
variations in load are few or minor in nature. 
school.edhole.com
5 
Failure Theories 
i. Maximum-Normal Stress Theory 
 This theory states that failure occurs whenever 
the largest principal stress equals the strength. 
 Suppose the principal stresses are ordered as: 
 Then if yielding is the criteria of failure, then failure 
occurs whenever: 
where: 
tensile yield stress 
= 
yt 
S 
 If ultimate tensile strength is used (in case of brittle 
materials), failure occur whenever: 
where: 
Principal 
Element 
1 2 3 s >s >s 
yt yc ³ S £ -S 1 3 s or s 
compressive yield stress 
= 
yc 
S 
ut uc ³ S £ -S 1 3 s or s 
tensile ultimate stress 
= 
compressive ultimate stress 
= 
ut 
S 
uc 
S 
Pure tension 
Pure torsion 
Note: For pure torsion s1 = t = s3 and s2 = 0. This 
means that the part fails in torsion when t = Sy. But 
experiments show that a part in torsion will deform 
at about 60% of the yield strength. This is one of 
the reasons the maximum-normal stress theory is 
not recommended. 
school.edhole.com
Failure Theories 
ii. Maximum-Shear Stress Theory 
 This theory is used only in the ductile materials. 
 It states that yielding begins whenever the maximum shear stress becomes equal to 
the maximum shear stress in a tension test specimen of the same material when that 
specimen begins to yield. 
6 
2 (for simple tension) 
t = 
s 
max 1 
t s s 
( ) 2 (for pure torsion) 
= - 
max 1 3 
 The maximum-shear stress theory predicts that failure will occur whenever: 
t s s s s 
max or 
 Shear yield strength is given by: 
y 
y S 
S 
= - 1 2 
³ - ³ 1 3 
2 2 
sy y S = 0.5S school.edhole.com
a) both volume change 
and angular distortion 
 For figure (a): 
 For unit cube, the work done in any of the principal 
(1 2 )[ 2 ( )] (2) 1 2 2 3 1 3 
7 
Failure Theories 
iii. The Distortion-Energy Theory 
 This theory is called the shear-energy theory. 
 It is used also for ductile materials. 
 Like the maximum-shear stress theory, this 
theory is employed to define the beginning of 
yield. It predicts that yielding will occur 
whenever the distortion-energy in a unit volume 
equals the distortion energy in the same volume 
when uniaxially stressed to the yield strength. 
 The distortion energy is obtained by subtracting 
equation (5) from equation (2): 
= 1 
+ ¢ 
3 
n s 
¢ = - + - + - 
E 
 So yielding is predicted to occur when: 
y school.edsh¢ ³oS le.com 
 Shear yield strength is given by: 
b) volume change c) distortion without 
volume change 
directions is: , where n= 1,2,3 
 The total strain energy is: or 
U = E s 2 
+s +s 2 
- n s s +s s +s s 
1 3 
 The average value savg: 
 The remaining stress, (s1-savg), (s2-savg), (s3-savg) will 
produce angular distortion, figure (c). Substituting (savg 
for s1, s2, s3) in equation (2) gives the amount of 
strain energy producing only volume change. 
s 2 = s +s +s 3 avg 
 Substituting in equation (4) 
gives: 
1 2 3 s >s >s 
2 (1) n n n U =s e 
1 2 3 U =U +U +U 
[ 2( )] (5) 
= 1 - 2 
n s +s +s + s s +s s +s s 
v 1 6 
1 2 2 3 1 3 
2 
3 
2 
2 
2 
E 
U 
( ) 3 (3) 1 2 3 s = s +s +s avg 
(3 2 2 )(1 2 ) (4) 
v U = s E - n avg 
[( ) ]2 
1 2 3 
2 
2 
where, [( ) 2 
( ) 2 
( ) 2 
] 2 
1 2 
2 3 
3 1 
2 
d 
s s s s s s s 
U 
sy y S = 0.577S
8 
Factor of Safety for each 
Failure Theory 
 For maximum-normal stress theory 
n = S n = - 
S 
= = - 
s s 
or (for ductile materials) 
s y s y 
n S n S 
1 3 
s s 
or (for brittle materials) 
s u s u 
1 3 
 For maximum-shear stress theory 
( ) 1 3 = s -s s y n S 
 For the distortion-energy theory: 
= ¢ s y n S 
school.edhole.com 
s 
¢ = - + - + - 
where, s [( s s ) 2 
( s s ) 2 
( s s 
)2 ] 2 
1 2 2 3 
3 1
9 
Example 
A material has a yield strength of 600 MPa. Compute the fator of safety for each of the 
failure theories for ductile materials. Use the following stress states: 
a)- s1 = 420 MPa: s2 = 420 MPa, s3 = 0 
b)- s1 = 420 MPa, s2 = 180 MPa, s3 = 0 
c)- s1 = 420 MPa, s2 = 0 MPa, s3 = -180 MPa 
d)- s1 = 0 MPa, s2 = -180 MPa, s3 = -420 MPa. 
school.edhole.com
9 
Example 
A material has a yield strength of 600 MPa. Compute the fator of safety for each of the 
failure theories for ductile materials. Use the following stress states: 
a)- s1 = 420 MPa: s2 = 420 MPa, s3 = 0 
b)- s1 = 420 MPa, s2 = 180 MPa, s3 = 0 
c)- s1 = 420 MPa, s2 = 0 MPa, s3 = -180 MPa 
d)- s1 = 0 MPa, s2 = -180 MPa, s3 = -420 MPa. 
school.edhole.com

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  • 1. Top School in Delhi NCR :By school.edhole.com
  • 2. 2 Section IV Failures Due to Static Loading school.edhole.com
  • 3. 3 Talking Points  Static Loading?  Failure Theories:  Maximum-Normal Stress Theory  Maximum-Shear Stress Theory  The Distortion-Energy Theory  Factor of Safety for each Failure Theory school.edhole.com
  • 4. 4 ?Static Loading  Static Load is a stationary force or moment acting on a member.  Stationary means that the force or moment does not change in magnitude.  Sometime the load is assumed to be static when it is known that some variation to be expected. Such assumptions are made to simplify the design computations when variations in load are few or minor in nature. school.edhole.com
  • 5. 5 Failure Theories i. Maximum-Normal Stress Theory  This theory states that failure occurs whenever the largest principal stress equals the strength.  Suppose the principal stresses are ordered as:  Then if yielding is the criteria of failure, then failure occurs whenever: where: tensile yield stress = yt S  If ultimate tensile strength is used (in case of brittle materials), failure occur whenever: where: Principal Element 1 2 3 s >s >s yt yc ³ S £ -S 1 3 s or s compressive yield stress = yc S ut uc ³ S £ -S 1 3 s or s tensile ultimate stress = compressive ultimate stress = ut S uc S Pure tension Pure torsion Note: For pure torsion s1 = t = s3 and s2 = 0. This means that the part fails in torsion when t = Sy. But experiments show that a part in torsion will deform at about 60% of the yield strength. This is one of the reasons the maximum-normal stress theory is not recommended. school.edhole.com
  • 6. Failure Theories ii. Maximum-Shear Stress Theory  This theory is used only in the ductile materials.  It states that yielding begins whenever the maximum shear stress becomes equal to the maximum shear stress in a tension test specimen of the same material when that specimen begins to yield. 6 2 (for simple tension) t = s max 1 t s s ( ) 2 (for pure torsion) = - max 1 3  The maximum-shear stress theory predicts that failure will occur whenever: t s s s s max or  Shear yield strength is given by: y y S S = - 1 2 ³ - ³ 1 3 2 2 sy y S = 0.5S school.edhole.com
  • 7. a) both volume change and angular distortion  For figure (a):  For unit cube, the work done in any of the principal (1 2 )[ 2 ( )] (2) 1 2 2 3 1 3 7 Failure Theories iii. The Distortion-Energy Theory  This theory is called the shear-energy theory.  It is used also for ductile materials.  Like the maximum-shear stress theory, this theory is employed to define the beginning of yield. It predicts that yielding will occur whenever the distortion-energy in a unit volume equals the distortion energy in the same volume when uniaxially stressed to the yield strength.  The distortion energy is obtained by subtracting equation (5) from equation (2): = 1 + ¢ 3 n s ¢ = - + - + - E  So yielding is predicted to occur when: y school.edsh¢ ³oS le.com  Shear yield strength is given by: b) volume change c) distortion without volume change directions is: , where n= 1,2,3  The total strain energy is: or U = E s 2 +s +s 2 - n s s +s s +s s 1 3  The average value savg:  The remaining stress, (s1-savg), (s2-savg), (s3-savg) will produce angular distortion, figure (c). Substituting (savg for s1, s2, s3) in equation (2) gives the amount of strain energy producing only volume change. s 2 = s +s +s 3 avg  Substituting in equation (4) gives: 1 2 3 s >s >s 2 (1) n n n U =s e 1 2 3 U =U +U +U [ 2( )] (5) = 1 - 2 n s +s +s + s s +s s +s s v 1 6 1 2 2 3 1 3 2 3 2 2 2 E U ( ) 3 (3) 1 2 3 s = s +s +s avg (3 2 2 )(1 2 ) (4) v U = s E - n avg [( ) ]2 1 2 3 2 2 where, [( ) 2 ( ) 2 ( ) 2 ] 2 1 2 2 3 3 1 2 d s s s s s s s U sy y S = 0.577S
  • 8. 8 Factor of Safety for each Failure Theory  For maximum-normal stress theory n = S n = - S = = - s s or (for ductile materials) s y s y n S n S 1 3 s s or (for brittle materials) s u s u 1 3  For maximum-shear stress theory ( ) 1 3 = s -s s y n S  For the distortion-energy theory: = ¢ s y n S school.edhole.com s ¢ = - + - + - where, s [( s s ) 2 ( s s ) 2 ( s s )2 ] 2 1 2 2 3 3 1
  • 9. 9 Example A material has a yield strength of 600 MPa. Compute the fator of safety for each of the failure theories for ductile materials. Use the following stress states: a)- s1 = 420 MPa: s2 = 420 MPa, s3 = 0 b)- s1 = 420 MPa, s2 = 180 MPa, s3 = 0 c)- s1 = 420 MPa, s2 = 0 MPa, s3 = -180 MPa d)- s1 = 0 MPa, s2 = -180 MPa, s3 = -420 MPa. school.edhole.com
  • 10. 9 Example A material has a yield strength of 600 MPa. Compute the fator of safety for each of the failure theories for ductile materials. Use the following stress states: a)- s1 = 420 MPa: s2 = 420 MPa, s3 = 0 b)- s1 = 420 MPa, s2 = 180 MPa, s3 = 0 c)- s1 = 420 MPa, s2 = 0 MPa, s3 = -180 MPa d)- s1 = 0 MPa, s2 = -180 MPa, s3 = -420 MPa. school.edhole.com