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Question

The critical radius (in $nm$, rounded off to one decimal place) of nickel nucleus during solidification at $1673 \text{ K}$ is ________. 

Given: Enthalpy of fusion of nickel = $2.65 \times 10^9 \text{ J.m}^{-3}$; 

Liquid-solid interfacial energy = $0.5 \text{ J.m}^{-2}$, and 

Equilibrium melting temperature of nickel = $1728 \text{ K}$.

This solution outlines the calculation for the critical radius of a nickel nucleus during solidification, utilizing fundamental principles of nucleation theory.

Critical Radius Formula

The critical radius ($r_c$) for homogeneous nucleation in a liquid is determined by the balance between the reduction in volume free energy and the increase in interfacial energy. The formula is:

$r_c = \frac{2 \sigma T_m}{\Delta H_f \Delta T}$

Where:

  • $\sigma$ represents the liquid-solid interfacial energy ($0.5 \text{ J.m}^{-2}$).
  • $T_m$ is the equilibrium melting temperature ($1728 \text{ K}$).
  • $\Delta H_f$ denotes the enthalpy of fusion ($2.65 \times 10^9 \text{ J.m}^{-3}$).
  • $\Delta T$ is the degree of undercooling, calculated as $T_m - T$.

Solidification Parameters

The problem provides the following data for nickel:

  • Interfacial energy ($\sigma$): $0.5 \text{ J.m}^{-2}$
  • Equilibrium melting temperature ($T_m$): $1728 \text{ K}$
  • Enthalpy of fusion ($\Delta H_f$): $2.65 \times 10^9 \text{ J.m}^{-3}$
  • Solidification temperature ($T$): $1673 \text{ K}$

Steps to Calculate Critical Radius

Step 1: Calculate the undercooling ($\Delta T$).

The undercooling is the difference between the equilibrium melting temperature and the actual solidification temperature.

$\Delta T = T_m - T = 1728 \text{ K} - 1673 \text{ K} = 55 \text{ K}$

Step 2: Substitute known values into the critical radius formula.

Using the formula $r_c = \frac{2 \sigma T_m}{\Delta H_f \Delta T}$:

$r_c = \frac{2 \times (0.5 \text{ J.m}^{-2}) \times (1728 \text{ K})}{(2.65 \times 10^9 \text{ J.m}^{-3}) \times (55 \text{ K})}$

Step 3: Perform the calculation.

Calculate the numerator:

$2 \times 0.5 \times 1728 = 1728 \text{ J.m}^{-2}\text{.K}$

Calculate the denominator:

$2.65 \times 10^9 \times 55 = 145.75 \times 10^9 = 1.4575 \times 10^{11} \text{ J.m}^{-3}\text{.K}$

Now, divide the numerator by the denominator:

$r_c = \frac{1728 \text{ J.m}^{-2}\text{.K}}{1.4575 \times 10^{11} \text{ J.m}^{-3}\text{.K}} \approx 1.1856 \times 10^{-8} \text{ m}$

Step 4: Convert the radius to nanometers ($nm$) and round.

To convert meters to nanometers, multiply by $10^9$ ($1 \text{ m} = 10^9 \text{ nm}$):

$r_c \approx 1.1856 \times 10^{-8} \text{ m} \times \frac{10^9 \text{ nm}}{1 \text{ m}} \approx 11.856 \text{ nm}$

Rounding to one decimal place, the critical radius is $11.9 \text{ nm}$. This value is consistent with the expected range.

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Important Questions from Solidification Directional Solidification

  1. A hypothetical binary eutectic phase diagram of A – B is shown below. An alloy with 5 wt.% B solidifies with no convection. Assuming steady state, the critical temperature gradient (in K $mm^{-1}$) required to maintain planar solidification front is: ________ (round off to nearest integer).
     

    Given:
    Diffusivity of B in liquid = $10^{-9}$ $m^2$ $s^{-1}$
    Velocity of solidification front = 4 $\mu m$ $s^{-1}$

  2. For a solid embryo in contact with a perfectly flat mould wall as shown in the schematic, the wetting angle $\theta$ is __________ degrees. 

    (Round off to one decimal place). 

    Given: 

    Surface tension between liquid and mould wall = $0.35 \text{ J.m}^{-2}$ 

    Surface tension between solid and mould wall = $0.02 \text{ J.m}^{-2}$ 

    Surface tension between liquid and solid = $0.40 \text{ J.m}^{-2}$

  3. The constitutional undercooling condition for a hypothetical binary alloy of A with solute B during solidification is shown in the figure along with its binary phase diagram. Based on these two schematics, one can conclude that the solute concentration in region X will be _______________ the average composition of the initial liquid phase.

  4. In continuous casting of steel, mould flux is used for ______________

  5. Single crystal turbine blades of nickel-based superalloys for aero-engines are manufactured using:

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