**Main page**

**About us**

**Engine Bearings Consulting**

**Advertising Opportunities**

# Materials Engineering

**Metals**

**Ceramics**

**Polymers**

**Composites**

**Fluids**

**Engine bearings**

**Materials Data**

**Materials Links**

**Index of SubsTech articles**

*to* Metals

*to* Metal properties and tests

**Dr. Dmitri Kopeliovich**

**Stress-Strain Diagram** expresses a relationship between a load applied to a material and the deformation of the material, caused by the load .

Stress-Strain Diagram is determined by **tensile test**.

Tensile tests are conducted in **tensile test machines**, providing controlled uniformly increasing tension force, applied to the specimen.

The specimen’s ends are gripped and fixed in the machine and its **gauge length L _{0}** (a calibrated distance between two marks on the specimen surface) is continuously measured until the rupture.

Test specimen may be round or flat in the cross-section.

In the round specimens it is accepted, that **L _{0} = 5 * diameter**.

The specimen deformation (**strain**) is the ratio of the increase of the specimen gauge length to its original gauge length:

**δ ****= (L – ****L _{0}**

**Tensile stress** is the ratio of the tensile load **F** applied to the specimen to its original cross-sectional area **S _{0}**:

**σ ****= F / ****S _{0}**

The initial straight line (**0P**)of the curve characterizes proportional relationship between the stress and the deformation (strain).

The stress value at the point **P** is called the **limit of proportionality**:

**σ**_{p}**= F _{P} / **

This behavior conforms to the **Hook’s Law**:

**σ ****= E*δ**

Where **E** is a constant, known as **Young’s Modulus **or** Modulus of Elasticity**.

The value of Young’s Modulus is determined mainly by the nature of the material and is nearly insensitive to the heat treatment and composition.

Modulus of elasticity determines **stiffness** - resistance of a body to elastic deformation caused by an applied force.

The line **0E** in the Stress-Strain curve indicates the range of **elastic deformation** – removal of the load at any point of this part of the curve results in return of the specimen length to its original value.

The elastic behavior is characterized by the **elasticity limit** (stress value at the point **E**):

**σ**_{el}**= F _{E} / **

For the most materials the points **P** and **E** coincide and therefore **σ**_{el}**=****σ**** _{p}**.

A point where the stress causes sudden deformation without any increase in the force is called **yield limit (yield stress, yield strength)**:

**σ**_{y}**= F _{Y} / **

The highest stress (point **Y**** _{U}**) , occurring before the sudden deformation is called

The lower stress value, causing the sudden deformation (point **Y**** _{L}**) is called

The commonly used parameter of yield limit is actually lower yield limit.

If the load reaches the yield point the specimen undergoes plastic deformation – it does not return to its original length after removal of the load.

Hard steels and non-ferrous metals do not have defined yield limit, therefore a stress, corresponding to a definite deformation (0.1% or 0.2%) is commonly used instead of yield limit. This stress is called **proof stress **or **offset yield limit (offset yield strength): **

**σ**_{0.2%}**= F _{0.2%} / **

The method of obtaining the proof stress is shown in the picture.

As the load increase, the specimen continues to undergo plastic deformation and at a certain stress value its cross-section decreases due to “necking” (point **S** in the Stress-Strain Diagram). At this point the stress reaches the maximum value, which is called **ultimate tensile strength** (**tensile strength**):

**σ**_{t}**= F _{S} / **

Continuation of the deformation results in breaking the specimen - the point B in the diagram.

The actual Stress-Strain curve is obtained by taking into account the true specimen cross-section instead of the original value.

Other important characteristic of metals is **ductility** - ability of a material to deform under tension without rupture.

Two ductility parameters may be obtain from the tensile test:

**Relative elongation ** - ratio between the increase of the specimen length before its rupture and its original length:

**δ ****= (****L**_{m}**– ****L _{0}**

Where **L _{m}**– maximum specimen length.

**Relative reduction of area - **ratio between the decrease of the specimen cross-section area before its rupture and its original cross-section area**:**

**ψ****= (****S _{0}**

Where **S _{min}**– minimum specimen cross-section area.

to top

http://www.virginia.edu/bohr/mse209/chapter6.htm

http://www.eng.auburn.edu/~wfgale/intro_metals/toc.htm

http://people.clarkson.edu/~rasmu/ES-260/Chapter_07.ppt

http://me.queensu.ca/courses/mech412/Notes/Review1.ppt

http://www.nde-ed.org/EducationResources/CommunityCollege/
Materials/Introduction/introduction.htm

http://www.ame.arizona.edu/courses/ame324b/l04.pdf

Except where otherwise noted, this work is licensed under a Creative Commons Attribution-Noncommercial-Share Alike 3.0 License