mmf experiment no 1

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MECHANICS OF METAL FORMING Jayesh Desai Page 1 EXPERIMENT NO: 1 AIM: Basics of metal forming Q-1 State the fundamental conditions for stress stress relations in plastic deformation. Ans…. The fundamental conditions for stress and strain ar e as follows. (1) in any plastic deformation process the work done is always positive. For example-if a specimen is extended, positive work is done, if it is c ompressed again positive work is done. (2) Plastic deformation takes place only when the stress incremen t vector at a point on the yield surface is directed outside t he yield surface. (3) If the body is in plastic state i.e. the str ess point is on the yield surface and the stress increment is directed along the ta ngent to the yield surface, or the stress point simply moves on the yield surface, then no plastic deformation on take place. Q-2 Explain the normality rule related to plastic stress strain relation. Ans…. the strain increment or strain rate in plastic deformation are proportional to the corresponding deviator stress components. From the plastic stress strain condition it is clear that the angle b etween the stress vector and the strain vector must always be acute only then the p lastic work done is al ways positive. From the second and third conditions it is clear that the stress increment may be in any direction pointing outside the yield surface, t he strain increment vector should always be directed along the normal to the yield surface at the point of application of stress increment, which is also the direction of deviator component of stress tensor. This is called the normality rule. Q-3 Differentiate following related to plastic stress strain relations. (a) rigid perfectly plastic material. (b) rigid work hardening material. (c) elastic perfectly plastic material. (d) elastic work hardening material. Ans…… If the material does not work harden it is called rigid perfectly plastic material. If the material does work harden it is called rigid hardening material. If the elastic deformation taken into account and material does not work harden it is called elastic perfectly plastic mat erial. If the material does work harden in elastic deformation it is called elastic work hardening material. The difference is illustrated in fig idealized stress strain relations.

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MECHANICS OF METAL FORMING

Jayesh Desai Page 1

EXPERIMENT NO: 1

AIM: Basics of metal forming

Q-1 State the fundamental conditions for stress stress relations in

plastic deformation.

Ans…. The fundamental conditions for stress and strain are as follows.

(1)  in any plastic deformation process the work done is always positive. For example-if a

specimen is extended, positive work is done, if it is compressed again positive work is done.

(2)  Plastic deformation takes place only when the stress increment vector at a point on

the yield surface is directed outside the yield surface.

(3)  If the body is in plastic state i.e. the stress point is on the yield surface and the stressincrement is directed along the tangent to the yield surface, or the stress point simply

moves on the yield surface, then no plastic deformation on take place.

Q-2 Explain the normality rule related to plastic stress strain

relation.Ans…. 

the strain increment or strain rate in plastic deformation are proportional to the

corresponding deviator stress components.

From the plastic stress strain condition it is clear that the angle between the stress

vector and the strain vector must always be acute only then the plastic work done is always

positive.From the second and third conditions it is clear that the stress increment may be in

any direction pointing outside the yield surface, the strain increment vector should always be

directed along the normal to the yield surface at the point of application of stress increment,

which is also the direction of deviator component of stress tensor. This is called the normality

rule.

Q-3 Differentiate following related to plastic stress strain relations.

(a) rigid perfectly plastic material.

(b) rigid work hardening material.

(c) elastic perfectly plastic material.(d) elastic work hardening material.

Ans…… If the material does not work harden it is called rigid perfectly plastic material.

If the material does work harden it is called rigid hardening material.If the elastic deformation taken into account and material does not work harden it is

called elastic perfectly plastic material.

If the material does work harden in elastic deformation it is called elastic work 

hardening material.

The difference is illustrated in fig idealized stress strain relations.

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Q-4 Explain plastic stress strain relation according to prantl-reuss

and levy-von mises relations.Ans…… 

Prentl-Reuss relations

The relationship between stress and strain increments dɛpij were first derived by Prantle in

1924 for plane strain deformation. Later these were generalised by Reuss. According toPrantle-Reuss relations the components of strain increments are proportional to corresponding

stress deviator components.

dɛpij ∞  σij …......................... (1) 

In expanded from the above eqn may be written as given below.

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dɛp11 ∞ σ11 ……………………..(2) 

dɛp22 ∞ σ22 ……………………..(3)

dɛp33 ∞ σ33 ……………………..(4)

dɛp12 ∞ σ12 ……………………..(5)

dɛp23 ∞ σ23 ………………………(6) 

dɛ p31 ∞ σ31 ………………………(7) 

the relations may be written as,

dɛpij ∞ dΦσij ……………………….(8) 

where dΦ is a factor of proportionality. These relations may be put in the following form.

dɛpij = (3/2)( dɛ

pij /σ)σij ……………………….(8) 

Levy-Von Mises relations 

The levy-von mises relations are similar to that of Prantl-Reuss. In these relations

the elastic increments are neglected .Its taken that strain increments are entirely

plastic increments. Hence

dɛpij = (3/2)( dɛ

pij /σ)σij …………………………(9) 

and also σ = σ0 

Stress Strain relations

The relationship between stresses and plastic strain rates may be written as below.

ɛpij = Φσij ………………………….(10) 

In the expanded form these may be written as

ɛp11 ∞ Φσ11

 = Φ(2σ11- σ22 –  σ33)/3  …………………………..(11) 

ɛ p22 ∞ Φσ22   = Φ(2σ22- σ11 –  σ33)/3  …………………………..(12) 

ɛp33 ∞ Φσ33

  = Φ(2σ33- σ11 –  σ22)/3  …………………………..(13) 

ɛp12 = Φσ12  = Φσ12  ……………………………(15) 

ɛp23 = Φσ23  = Φσ23  ……………………………(16) 

ɛp31 = Φσ31  = Φσ31  ……………………………(17) 

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Here Φ is the factor of proportionality. It is not constant. Multiplying both sides of eqn(11) by

it self we get Φ as below.

ɛpij  ɛ

pij = Φ2 σij σij

also

σij σij = 2 K2 = 2/3 σ0

Therefore

Φ = √ ɛ ij ɛ ij /  √2 K ………………………...(18) 

Q-5 What do you meant by yield condition?

Ans…… 

A yield criterion is a postulated mathematical expression of the states of stress that will cause

yielding. The most general form is

f (σx ,σy ,σz ,τyz ,τzx ,τxy ) = C …………………………(1) 

For isotropic materials, this can be expressed in terms of principal stresses as

f (σ1,σ2,σ3) = C ………………………….(2) 

Formost isotropic ductilemetals the following assumptions are commonlymade:

1. The yield strengths in tension and compression are the same. That is, any

Bauschinger∗ effect is small enough so it can be ignored.

2. The volume remains constant during plastic deformation.

3. The magnitude of the mean normal stress,

σm = σ1 + σ2 + σ3/3 …………………………….(3) does not affect yielding.

The yield criteria to be discussed involve these assumptions. Effects of temperature,

prior straining, and strain rate will be discussed in later chapters.The assumption that yielding is independent of σm is reasonable because defor -mation usually occurs by slip or twining, which are shear mechanisms. Therefore the

yield criteria for isotropic materials have the form

f [(σ2 − σ3), (σ3 − σ1), (σ1 − σ2)] = C ………………………….(4)

This is equivalent to stating that yielding depends only on the size of theMohr’scircles 

and not on their positions. Figure 2.1 shows this. If a stress state σ1,σ2,σ3 will cause

yielding, another stress state,

σ1 = σ1 - σm

σ2 = σ2 - σm

σ3 = σ3 - σm 

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that differs only by σm,will also cause yielding. The stresses σ1, σ2 , σ3 are called deviatoric

stresses.

Q-6 Derive the relationship between yield strength in shear and yield

strength in tension according to Von-Mises hypothesis.

Ans…. 

Von-Mises criteria takes into account from the eqn of yield criteria.

II = K

2 …………………………..(1) 

Wherw K is the constant which may be rekated to material properties. The details are

discussed below.

 A stressed metal body reaches the yield point if the following eqn is satisfied.

(σ11 - σ22)2 + (σ22 –  σ33)2 + (σ33 –  σ11)2 +6 (σ122

+ σ232

  + σ312

 ) = 6K2 ………..(2) 

In the principal stresses σ1, σ2 and σ3 , The eqn (1) reduces to the following form.

(σ1 - σ2)2 + (σ2 –  σ3)2 + (σ3 –  σ1)2= 6K2 ……………………(3) 

The value of K may be determined from the uniaxial tension or compression test, in which

case, we may take that σ1ǂ 0, while the other two principal stresses equal to zero. We put

these value in eqn (3) . also we know that yielding takes place only when σ1 = σ0 = yield

strength of material in tension thus,

2 σ12 = 2 σ0

2= 6K

2 ………………………….(4) 

Therefore,

K= σ0/√3 ………………………….(5) 

Value of K may also be determined by experimenting with a different state of stress. Thus by

subjecting a thin tube to torsion we may create a condition for pure shear.by increasing the

torsion and hence shear stress the material of the tu be is brought to the yield point. Let σ12 be

the shear stress due to the torsion and let Ʈ 0 be the yield strength of the material in shear . by

substituting σ12 = Ʈ 0 and all other stress components equal to eqn(2), we get the following .

K = Ʈ 0 = yield strength of material in shear……………………..(6) 

From eqn (4) and (5) it is obvious that,

Ʈ 0 = σ0/√3 ………………………….(7) 

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Eqn (7) gives a relationship between the yield strength of material in shear to its yield

strength in tension.

Q-7 Derive the relationship between yield strength in shear and yieldstrength in tension according to Tresca’s hypothesis.

Ans…. 

 A metal body reaches the yield point when the maximum shear stress in the body

reaches the value equal to the yield strength of the metal in shear.

If the stress state is given by three principal stresses σ1, σ2 and σ3 the maximum shear

stress are as follows.

Ʈ 1 max = ½ (σ1 - σ2)

Ʈ 2 max = ½ (σ2 –  σ3)

Ʈ 3 max = ½ (σ3 –  σ1)

Out of these three we can evaluate the greatest value of shear stress if we know the

relative magnitudes of the principal stresses. Let us takes that σ1> σ2 > σ3 then the greatest

value of shear stress is givaen by

Ʈ max = ½ (σ1 –  σ3)

According to tresca’s hypothesis the metal body will be in plastic state if  

½ (σ1 –  σ3) = Ʈ 0

Where Ʈ 0= yield strength of the material in shear.

In tension test we may take that σ1ǂ 0 while all other stress components are zero.The yielding

occurs when σ1 = σ0 = yield strength of material in tension. Also we know that in case of 

uniaxial tension the greatest value of shear stress is equal to half the tensile stress. Therefore

at the yield point,

Ʈ 0 = σ0/2 ………………………….(1)

Thus according to tresca’s hypothesis , the yield strength in shear is equal to half the yield strength in tension while according to van-mises its equal to

Ʈ 0 = σ0/√3. 

Tresca’s hypothesis may also be written in the gener alised form as given below.

[(σ1 - σ2)2 - 4 Ʈ 02

] [(σ2 –  σ3)2- 4 Ʈ 02

] [(σ3 –  σ1)2- 4 Ʈ 02

]= 6K2 …(2) 

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Q-8 Give out the graphical 3 dimensional representation of yield

crieteria.

Ans… 

The graphical representation gives a better understanding of two yield criteria

von-mises and tresca’s hypothesis. For convenience we take the coordinate axes along the

three principal stresses σ1, σ2 and σ3 .

In these coordinate system, any stress state given by a set of three principal

stresses σ1, σ2 and σ3 is represented by a point. Von mises yield criteria is represented by a

cylindrical surface while tresca’s criteria represented by hexagonal prism. 

Tresca’s hexagonal prism is indicated inside von mises dylinder bcoz we havetaken that yield strength in tension/compression is same for both hypothesis.

Von mises cylinder as well as tresca’s prism have same axis which equally inclined to the

coordinate axes. The direction consis of axis of von-mises cylinder rae 1/ √3, 1/ √3, 1/ √3 . theinclination of this axis with coordinate axes is cos-1 (1/ √3)=54.7340

.The radius of von mises cylinder on the plane perpendicular to its axis is given by,

σ0 sin (cos-1

 (1/ √3) = (√2 /√3) σ0 = √2 K……………………………(1) 

Any point on this axis of the cylinder represents a stress in which the three

principal stresses are equal, which is case of hydrostatic pressure .a line perpendicular to the

axis represents the deviator part of stress tensor. Let us take that stress state is represented bypoint P ( fig). The vector OP presents the total stress vector. It is divided into two

components OR and RP. The vector OR represents the hydrostatic pressure and RP is the

deviator component.

Fig- graphical representation of yield criteria

If the point lies inside von-mises cylinder, the material is elastic or a rigidbody. It becomes plastic only when the point P lies on the surface of cylinder. i.e

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when the stress state satisfies . points outside the cylinder are not defined. It is taken

that the material will suffer plastic deformation when P is on the cylinder and stress

increment is directed outside the cylinder. A similar discussion applies to tresca’shexagonal prism as well.

 Both the yield conditions show that hydrostatic pressure, whatever its value,cannot bring a metal body to the yield point. Because in that condition the stress point 

will lie on the axis of yield surface and not its surface.

Fig- Von mises’s yield condition & stress at a point 

Now if the stress point P lies on the yield surface and stress increment is directed

tangentially to yield surface we shall only be moving from one state of yielding to another

state of yielding and hence no plastic deformation occurs, plastic deformation occurs only

when the incremental stress vector is directed out side von-mises ‘ cylinder or tresca’shexagonal prism.

Q-9 Explain about any one factor which affect the yield strength.

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Ans……. 

The yield strength of the of a metal or alloy is affected by following factors.

(1)  Strain hardening.

(2)  Strain rate.(3)  Temperature of metal and microstructure.

(4)  Hydrostatic pressure.

Effect of hydrostatic pressure

Hydrostatic pressure may affect the following properties of metals and hence their

formability.

(1)  Ductility

(2)  Yield strength of flow stress.(3)  Strain hardening and strain rate index.

Experiments of bridgeman have shown that hydrostatic pressure does not lead to

plastic deformation. However, hydrostatic pressure increases the ductility and formability of metals and alloys. The phenomenon of increased ductility with hydrostatic pressure is also

called pressure indused ductility.

Fig- effect of hydrostatic pressure on yield strength of quenched and tempered AISI4330 steel

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Even brittle materials may be plastically deformed under suitable hydrostatic

pressure. Materials in which the plastic deformation leads to change in volume, the yieldstrength may be affected by hydrostatic pressure. Spitzig have shown that yield strength of 

quenched and tempered AISI 4310 and 4330 steels is affected by hydrostatic pressure.

In Fig shows the effect of hydrostatic pressure on the yield strength of 4330 steel.Both the steels show increase in volume during plastic deformation as well as increase in

yield strength under hydrostatic pressure. Very few researchers have attempt to determine the

effect of hydrostatic pressure on strain hardening and strain rate effect indices. According tospitzig , there is no effect of hydrostatic pressure on the strain hardening index.

Q-10 why most of metals obey von-mises yield criteria? Explain it.

Ans….. 

Several methods have been used to verify the two criteria of yielding metals.According to them we have take the taylor and quinney. In this method a tube of metal to be

tested , is loaded by a couple to produce shear stress and direct axial force is applied metal tobe tested , is loaded by a couple to produce shear stress and direct axial force is applied to

produce axial tension.

Thus different combinations of direct stress and shear stress values which can

 produce yielding of metal aer obtained. Let the axial force produce a direct axial stress σ andthe couple produce a shear stress Ʈ . The principal stresses σ1, σ2 and σ3 may be determined as

given below.

σ3 = 0 …………………………..(1)  

and

σ1, σ2 = σ/2 ± [ (  σ/2 )2+ Ʈ 2

]1/2 ………………………(2) 

now according to tresca’s hypothesis of yielding the maximum shear stress shouldbe equal to yield strength of metal in shear. In above case σ1 >  σ2 >  σ3 .

The greatest shear stress is given by

( σ1- σ2 ) / 2 = [ (  σ/2 )2+ Ʈ 2

]1/2

Therefore,

[ (  σ/2 )2+ Ʈ 2

]1/2

= Ʈ 0 = σ0 /2

Taking square of both sides and rearranging the terms we get,

(  σ/σ0)2

+ 4 (  Ʈ /σ0)2  = 1 …………………… (3) 

It is an eqn of ellipse. Similarly by putting σ and Ʈ in von-mises hypothesis we get

(  σ/σ0) + 3 (  Ʈ /σ0)2  = 1 ………………………………(4) 

This is also an eqn of ellipse eqn (2) and (3) are plotted in fig for sake of compression.

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Fig. – Inclined plane in space of principal stresses.

From above three equations we can also solve for the three variables n12 ,  n2

2 and n32. let us

take that

1 1 1

σ 1  σ 2 σ 3  = ∆ 

σ 12  σ 2

2  σ 32 

Now we can determine n12 ,  n2

2 and n32 as given below.

1 1 1

n12

= 1/ ∆  σ 2  σ 3 σ n σ 2

2  σ 3

2  σ n

2+ σ s

1 1 1

n2

2

  = 1/ ∆ σ 3  σ n σ 1 σ 32  σ n

2+ σ s

2  σ 12 

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1 1 1

n32  = 1/ ∆ σ 3  σ n σ 2 

σ n2

+ σ s2  σ 1

2  σ 22 

The above equations for n12 ,  n2

2 and n32 can be written in the following form after

simplification.

[ σ n_

1/2 ( σ 2 + σ 3 ) ]

2+ σ s

2= n1

2( σ 2

  _  σ 3 ) ( σ 2

  _σ 3 ) + 1/4 ( σ 2

  _σ 3 )

2 ……(4) 

[ σ n_

1/2 ( σ 1 + σ 3 ) ]

2+ σ s

2= n2

2( σ 2

  _  σ 3 ) ( σ 2

  _σ 1 ) + 1/4 ( σ 3

  _σ 1 )

2…….(5) 

[ σ n_

1/2 ( σ 1 + σ 2 ) ]

2+ σ s

2= n3

2( σ 3

  _  σ 1 ) ( σ 3

  _σ 2 ) + 1/4 ( σ 1

  _σ 2 )

2…….(6) 

The Eqns (4) ,(5) and (6) are in fact equations of circles if we take σ n and  σ s as variables.

For instance the corresponding to Eqn, (4) has its centre [1/2 ( σ 2 + σ 3 ), 0] and radius equal

[( σ 2  _

  σ 3 ) ( σ 2  _

σ 3 ) + 1/4 ( σ 2  _

σ 3 )2]

1/2

Two dimensional Mohr’s Stress Cricle. 

Two dimensional cases arise, when the inclined plane is normal to X 1 or X  2 or X  3, forinstance, let the plane be normal to X 1, i.e. n1 = 0. The Eqn.(4) converts into a two

dimensional Mhor’s circle giving relationship between σ 2 and

 σ 3 . All the three two

dimensional-cases that arise when the inclined plane becomes normal to one of the axes are

discussed below.

When n1 = 0, Moher’s circle equation become

[ σ n_

1/2 ( σ 2 + σ 3 ) ]

2+ σ s

2= 1/4 ( σ 2

  _σ 3 )

2 …………………………………(7) 

Similarly When n2 = 0 , the inclined plane is normal to X  2 ,the equation for Moher’s stresscircle is given by following equation.

[ σ n _ 1/2 ( σ 1  + σ 3 ) ] 2 + σ s2 = 1/4 ( σ 3  _ σ 1 ) 2 …………………………………(8) 

Similarly When n2 = 0, Moher’s circle equation become 

[ σ n_

1/2 ( σ 1 + σ 2 ) ]

2+ σ s

2= 1/4 ( σ 1

  _σ 2 )

2 …………………………………(9) 

The Enq. (9) can be conveniently represented graphically as shown in Fig(3.6). now if  n1 

= cos θ then n2 = sin θ , n3 = 0. Therefore, the normal stress on the inclined plane (see Fig 3.6)

become,

σ n = σ 1 n12+ σ 2 n2

2

= σ 1 cos θ 2+ σ 2 sin θ 2 

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