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First, let’s start with the basics, and further we will drill down the various concepts of strength of materials, later on down the road.

**Classification of Engineering mechanics-**

Engineering mechanics is classified into three categories-

- Static
- Dynamic
- Mechanics of materials or strength of materials

**Static and Dynamic mechanics- **

Static and dynamic mechanics deals with the external effect on the rigid body with applied load. It can not tell about the internal effect that happens inside the body with applied load. The study of the non-deformative body comes under these mechanics, In general.

**Mechanics of Materials-**

Mechanics of materials deals with the Internal effect and deformations that are caused by the applied load. *Mechanics of materials are also known as Strength of Materials (SOM)*.

The study of a deformative body or change in shape with applied load, known as strength of materials and deals with the behavior of stresses and strains on the solid body with an applied load such as beams, columns and shaft.

**Why we study strength of materials-
**

As the name suggests, The study of materials’ strength deals with the **strength of materials**. It plays a very crucial role in designing the body or components such as engines, machines, bridges, flyovers, cranes, lifts, etc.

This can be used to-

- To evaluate the load applied to the body
- Select the material which can sustain the load

**SOM** is used to select the material and evaluate the strength of the materials as per the load about to be put on, to prevent the failure of the component with applied over time. As you know, when induced stress is gone beyond the material strength, the failure of the material occurs.

In general, the ability to withstand an applied load without failure or plastic deformation is known as the strength of the material.

Now, Let’s discuss the basics of SOM with its equations.

## Strength of materials basics with equations used-

Here are some basic definitions of SOM along with its equations-

**Stress-**

Stress is the internal resisting force developed in the body due to externally applied load. It is further denoted by σ.

The stress formula is given by-

Where P= Force. A= Area and the unit is- N/mm^{2}

**Strain-**

When an applied load causes deformation in the body, the deformation per unit length is called strain. It is denoted by ∈.

The strain formula is given by-

Where, δl= change in length, l= original length, and there is no unit of the strain.

**Stress-strain curve diagram-**

When the steel specimen is subjected to tensile load, the stress is directly proportional to the strain till the elastic limit, This is also known as Hook’s law.

The constant proportionally is known as young’s modulus law. It presents the slowness of this curve before the elastic limit. Upon loading it further, permanent deformation produces, and this behavior is known as strain hardening.

After further loading, the cross-sectional area of the specimen rapidly decreases and this phenomenon is known as necking.

And finally, the specimen reaches its point and gets fractured into cup and cone shapes.

**Modulus of elasticity-**

It is the ratio of stress in the body to the strain applied to the body. The unit of modulus of elasticity is – N/mm^{2}

The formula of Modulus of elasticity given by-

**Poisson Ratio-**

Poisson’s ratio is the ratio between lateral strain to the linear strain within elastic limit under direct loading. It is denoted by µ or 1/m.

The famous French mathematician Simeon Denis Poisson is the founder of the Poisson’s ratio in 1827.

The formula of Poisson’s ratio is given by-

**The volumetric strain of a rectangular body subjected to an axial load-**

Where, b= width, t=thickness, E=modulus of elasticity, 1/m= Poisson’s ratio

**The volumetric strain of a rectangular body subjected to three mutually perpendicular forces-**

Where, ∈x = Strain in x-direction, ∈y= Strain in y-direction, ∈z= strain in z-direction

**Bending Equation-**

Destruction in components due to applied load in any of the longitudinal planes is known as bending.

The bending equation is given by-

Where, M= bending moment, I= moment of inertia, σ= Bending stress, y= (D/2) distance from the neutral axis, E= modulus of elasticity, R= radius of curvature

**Torsional Equation-**

θτ

Where, T= torque, J= Polar moment of inertia, C= Torsional Rigidity, θ= Angle of twist, τ= shear stress, R= Radius of the circular shaft.

Here is the video guide to help you go deep into **Introduction to the strength of materials**–

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*Abhishek Tiwary is a blogger by passion and a Quality Engineer by profession. He completed his B.Tech degree in the year 2017. Now working in a reputed firm. He loves to share his knowledge with others.*