Skip to main content

Mechanics of Solids - short answer type questions from AMIE Exams (Winter 2017)

Write short notes on (4 marks each)

Generalised Hooke’s law

Hooke’s Law states that when a material is loaded within the elastic limit, the stress is proportional to the strain produced by the stress. This means the ratio of the stress to the corresponding strain is a constant within the elastic limit. This constant is known as Modulus of Elasticity or Modulus of Rigidity or Elastic Modulii.

Differential equation of equilibrium

The Small-Strain Stress-Strain Relations


{\varepsilon _{xx}} = \frac{{\partial {u_x}}}{{\partial x}}
{\varepsilon _{yy}} = \frac{{\partial {u_y}}}{{\partial y}}
{\varepsilon _{xy}} = \frac{1}{2}\left( {\frac{{\partial {u_x}}}{{\partial y}} + \frac{{\partial {u_y}}}{{\partial x}}} \right)

Simple Shear
{\varepsilon _{xy}} = \frac{1}{2}\left( {\frac{{\partial {u_x}}}{{\partial y}} + \frac{{\partial {u_y}}}{{\partial x}}} \right) = \frac{1}{2}\left( {\frac{{\partial {u_x}}}{{\partial y}}} \right)

Pure shear
{\varepsilon _{xy}} = \frac{1}{2}\left( {\frac{{\partial {u_x}}}{{\partial y}} + \frac{{\partial {u_y}}}{{\partial x}}} \right) = \frac{{\partial {u_x}}}{{\partial y}} = \frac{{\partial {u_y}}}{{\partial x}}

Tresca yield criteria

According to this theory, the failure of material will occur when the maximum shear stress in a material reaches the value of maximum shear stress in simple tension at the elastic limit. The maximum shear stress in the material is equal to half the difference between the maximum and minimum principal stress.

If σ₁, σ₂ and σ₃ are principal stresses at a point in material for which σt* is the principal stress in simple tension at the elastic limit, then

Max. shear stress in the material 
= Half of the difference of maximum and minimum principal stresses
\frac{1}{2}[{\sigma _1} - {\sigma _2}]

In the case of simple tension, at the elastic limit, the principal stresses are σt*, 0, 0

Max. shear stress in simple tension at elastic limit
\frac{1}{2}[{\sigma _t}^* - 0] = \frac{1}{2}{\sigma _t}^*

For the failure of the material
({\sigma _1} - {\sigma _3}) \ge {\sigma _t}^*

For design, the following equation should be used
({\sigma _1} - {\sigma _3}) = {\sigma _t}

Impact test

The capacity of a material to resist or absorb shock energy before it fractures is called its impact strength. The standard machine for impact testing is of the pendulum type (see figure). 


A notch is cut in the specimen, i.e. a standard test piece which struck under impact conditions by a heavyweight attached to the end of the pendulum. The test piece, i.e. specimen is held in an anvil (vice) and is broken by a single blow of the pendulum weight or hammer which is allowed to fall from a fixed starting point of a known height. The pendulum swings on after breaking the specimen and the height to which the pendulum rises on the other side are measured. 

Hardness test  

This is essentially the resistance of the surface of a material to deformation. We may note that there is no absolute scale for hardness. The commonly used tests for hardness are:
  • Brinell hardness test
  • Vickers hardness test
  • Rockwell hardness test
  • Rebound hardness test
Brinell Hardness Test
Ill this test a standard hardened steel ball of diameter D is pressed for about 10-15 seconds into the surface of the specimen by a gradually applied load P (see figure). 


The diameter of the indentation is measured after the load and ball are removed. The impression of the steel ball (indenter) so obtained, is measured to the nearest 0.2 mm with the help of a microscope.

The BHN number for some metals are
Lead: 4-8
Zinc: 25-40
Cast iron: 115-200
Nickel: 30-160
H.S.S.: 450-700

---
The study material for AMIE/B Tech/Junior Engineer exams is available at https://amiestudycircle.com 





Comments

Popular posts from this blog

Mechanics of Fluids (Solved Numerical Problems)

Numerical The surface Tension of water in contact with air at 20°C is 0.0725 N/m. The pressure inside a droplet of water is to be 0.02 N/cm² greater than the outside pressure. Calculate the diameter of the droplet of water. (7 marks) (AMIE Summer 2023) Solution Surface tension, σ = 0.0725 N/m Pressure intensity, P = 0.02 N/m 2 P = 4σ/d Hence, the Diameter of the dropd = 4 x 0.0725/200 = 1.45 mm Numerical Find the surface tension in a soap bubble of 40 mm diameter when the inside pressure is 2.5 N/m² above atmospheric pressure. (7 marks) (AMIE Summer 2023) Answer: 0.0125 N/m Numerical The pressure outside the droplet of water of diameter 0.04 mm is 10.32 N/cm² (atmospheric pressure). Calculate the pressure within the droplet if surface tension is given as 0.0725 N/m of water. (AMIE Summer 2023, 7 marks) Answer: 0.725 N/cm 2   Numerical An open lank contains water up to a depth of 2 m and above it an oil of specific gravity 0.9 for a depth of 1 m. Find the pressure intensity (i) at t...

Design of Electrical Systems (Solved Numerical Problems)

Important note There is something wrong with this question paper. It seems that instead of "Design of Electrical Systems" the IEI has given problems from "Electrical Machines". You should raise a complaint to director_eea@ieindia.org in this regard. Numerical A 120 V DC shunt motor draws a current of 200A. The armature resistance is 0.02 ohms and the shunt field resistance is 30 ohms. Find back emf. If the lap wound armature has 90 slots with 4 conductors per slots, at what speed will the motor run when flux per pole is 0.04 Wb?​ (AMIE Summer 2023, 8 marks) Solution The back EMF (E b ) of a DC motor can be calculated using the formula: E b = V - I a R a   Given: V = 120 V I a = 200 A R a = 0.02 ohms Substituting the values into the formula: E b = 120 − 200 × 0.02 = 120 − 4​ = 116 V Now, let's calculate the speed (N) at which the motor will run using the given flux per pole (φ p ). The formula to calculate the speed of a DC motor is: N = 60×E b /(P×φ p ) Wh...

Energy Systems (Solved Numerical Problems)

Wind at 1 standard atmospheric pressure and \({15^0}C\) has velocity of 15 m/s, calculate (i) the total power density in the wind stream (ii) the maximum obtainable power density (iii) a reasonably obtainable power density (iv) total power (v) torque and axial thrust Given: turbine diameter = 120 m, and turbine operating speed = 40 rpm at maximum efficiency. Propeller type wind turbine is considered. (AMIE Winter 2023) Solution For air, the value of gas constant is R = 0.287 kJ/kg.K 1 atm = 1.01325 x 105 Pa Air density \(\rho  = \frac{P}{{RT}} = \frac{{1.01325x{{10}^5}}}{{287}}(288) = 1.226\,kg/{m^3}\) Total Power \({P_{total}} = \rho A{V_1}^3/2\) Power density \(\begin{array}{l}\frac{{{P_{total}}}}{A} = \frac{1}{2}\rho {V_1}^3\\ = \frac{1}{2}(1.226){(15)^3}\\ = 2068.87{\mkern 1mu} W/{m^2}\end{array}\) Maximum power density \(\begin{array}{l}\frac{{{P_{\max }}}}{A} = \frac{8}{{27}}\rho A{V^3}_1\\ = \frac{8}{{27}}(1.226){(15)^3}\\ = 1226{\mkern 1mu} W/{m^2}\end{array}\) Assuming eff...