MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

 MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

Indian Institute of Technology Kanpur

Department of Materials Science and Engineering

MSE 626 Transport Phenomena

AY 2025-2026 Semester I

End Semester Examination Model Solutions



MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions





MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions



MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions



MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions
MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions




MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions



MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions

MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions


MSE 626: Transport Phenomena – End-Semester Examination: Model Solutions





Problem 1

Consider flow of liquid film over an inclined plane. A shell force balance is applied to a control volume of length L, thickness Δx and width W along the z direction.

The balance gives the equation:

(P0 − PL) ΔxW + (τxz|x − τxz|x+Δx) WL + ρ(LWΔx) g cosβ = 0

Since both ends of the inclined plane are open, P0 = PL.

Dividing by the control volume and taking the limit as Δx → 0:

− dτxz/dx + ρ g cosβ = 0

Therefore:

dτxz/dx = ρ g cosβ

Integrating:

τxz = ρ g cosβ x + C1

Using Newton's law of viscosity:

τxz = − μ dvz/dx

Thus:

− μ dvz/dx = ρ g cosβ x + C1

Integrating again:

vz = − (ρ g cosβ / 2μ) x² − (C1/μ)x + C2

Boundary Conditions

1. No slip at the wall of inclined plane: vz = 0 at x = δ

2. At free surface x = 0 the shear stress is zero.

Using these conditions:

C1 = 0

C2 = ρ g cosβ δ² / 2μ

Velocity Distribution

vz = (ρ g cosβ / 2μ)(δ² − x²)

or

vz = (ρ g cosβ δ² / 2μ)(1 − x²/δ²)

Maximum Velocity

vz,max = ρ g cosβ δ² / 2μ

Average Velocity

v̄z = (2/3) vz,max

Volumetric Flow Rate

Q = v̄z (δW)

Q = ρ g cosβ δ³ W / 3μ

Mass Flow Rate

ṁ = ρ Q

ṁ = ρ² g cosβ δ³ W / 3μ

Wall Shear Force

τxz at x = δ multiplied by wall area gives the total wall shear force.

Problem 2

Consider a slab with internal heat generation under steady state conditions.

From shell energy balance:

d²T/dx² + S/k = 0

Integrating:

dT/dx = − Sx/k + C1

Integrating again:

T = − Sx²/(2k) + C1x + C2

Boundary Conditions

Right face at x = L: T = 25°C

Left face at x = −L is insulated: dT/dx = 0

Solving gives constants C1 and C2.

The temperature profile and heat flux profile can then be plotted across the slab.

Problem 3

Emissive power of a black body:

Eb = σ T⁴

For temperature T = 5800 K and σ = 5.673 × 10⁻⁸ W/m²K⁴:

Eb = 5.673 × 10⁻⁸ × (5800)⁴

Eb = 64.198 × 10⁶ W/m²

Eb = 64.198 MW/m²

Problem 4

Radiation exchange between diffuse gray surfaces in an enclosure can be written as:

qi = (Eb,i − Ji) / ((1 − εi) / (εi Ai))

The radiosity equations for each surface are solved simultaneously to determine J1, J2 and J3.

Once radiosities are obtained, net heat transfer from each surface can be calculated.

Problem 5

Hydrogen diffusion through steel vessel is analyzed using steady state shell mass balance in spherical coordinates.

The governing equation becomes:

(1/r²) d/dr (r² NH) = 0

Integrating:

NH = C1 / r²

Using Fick's law:

JH = − DH-Fe dCH/dr

Integrating with boundary conditions at inner and outer radii gives concentration distribution.

The hydrogen molar flow rate through the spherical wall is:

WH = 2.63 × 10⁻⁵ mole of H per second

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