Heat Transfer Miscellaneous


  1. For the circular tube of equal length and diameter shown in figure below, the view factor F13 is 0.17. The view factor F12 in this case will be









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    1
    = 2
    r1

    and
    r3
    = 0.5
    l

    F13 = 0.17,
    F11 = 0,
    F11 + F12 + F13 = 1
    ∴ F12 = 1 – F13
    = 1 – 0 – 17 = 0.83

    Correct Option: D

    1
    = 2
    r1

    and
    r3
    = 0.5
    l

    F13 = 0.17,
    F11 = 0,
    F11 + F12 + F13 = 1
    ∴ F12 = 1 – F13
    = 1 – 0 – 17 = 0.83


  1. The properties of mercury at 300 K are: Density = 13529 kg/m³, cp = 0.1393 kJ/kgK, dynamic viscosity = 0.1523 × 10–2 Ns/m² and thermal conductivity = 8.540 W/mK. The Prandtl number of the mercury at 300 K is









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    Prandtl number =
    μCp
    K

    = 0.1523 × 10-2
    Ns
    ×
    0.1393 × 1000
    kJ
    = 0.0248
    8.54/mKkgK

    Correct Option: A

    Prandtl number =
    μCp
    K

    = 0.1523 × 10-2
    Ns
    ×
    0.1393 × 1000
    kJ
    = 0.0248
    8.54/mKkgK



  1. A coolant fluid at 30°C flows over a heated flat plate maintained at a constant temperature of 100°C. The boundary layer temperature distribution at a given location on the plate may be approximated as T = 30 + 70 expt(-y) where y(in m) is the distance normal to the plate and fis in °C. If thermal conductivity of the fluid is 1.0 W/mK, the local convective heat transfer coefficient (in W/m²K) at that location will be









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    Under steady state conditions
    Heat transfer by conduction = Heat transfer by convection

    ∴ -kA
    dT
    = h AΔT
    dy

    or -k
    dT
    = h ΔT
    dy

    or -k
    dT
    (30 + 70e-y) = h (100 - 30°)
    dy

    or -k
    δ
    (- 70e-y) = h × 70
    δy

    or – k
    ∴ -k (– 70 e0) = 70h
    or 70 k = 70 h
    But k = 1
    ∴ h = 1W/m²k
    Alternately
    hAΔ = kA
    dT
    dy

    or h(100 – 30) = k × (100 – 30)
    or h = k = 1 W/m²K

    Correct Option: B

    Under steady state conditions
    Heat transfer by conduction = Heat transfer by convection

    ∴ -kA
    dT
    = h AΔT
    dy

    or -k
    dT
    = h ΔT
    dy

    or -k
    dT
    (30 + 70e-y) = h (100 - 30°)
    dy

    or -k
    δ
    (- 70e-y) = h × 70
    δy

    or – k
    ∴ -k (– 70 e0) = 70h
    or 70 k = 70 h
    But k = 1
    ∴ h = 1W/m²k
    Alternately
    hAΔ = kA
    dT
    dy

    or h(100 – 30) = k × (100 – 30)
    or h = k = 1 W/m²K


Direction: Consider steady one-dimensional heat flow in a plate of 20 mm thickness with a uniform heat generation of 80 MW/m³. The left and right faces are kept at constant temperatures of 160°C and 120°C respectively. The plate has a constant thermal conductivity of 200 W/mK.

  1. The location of maximum temperature within the plate from its left face is









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    d²T
    +
    q0
    = 0
    dx²K

    ∴ T =
    - 1
    q0
    x² + C1x + C2......(i)
    2K

    At x = 0, T = 433 K
    ∴ C2 = 433
    At x = 20 × 10–3 m, T = 393 K.
    ∴ C1 = 200
    For maximum temperature,
    dT
    = 0
    dx

    q0x
    + C1 = 0
    K

    x = 5 × 10–3 = 5 mm

    Correct Option: C


    d²T
    +
    q0
    = 0
    dx²K

    ∴ T =
    - 1
    q0
    x² + C1x + C2......(i)
    2K

    At x = 0, T = 433 K
    ∴ C2 = 433
    At x = 20 × 10–3 m, T = 393 K.
    ∴ C1 = 200
    For maximum temperature,
    dT
    = 0
    dx

    q0x
    + C1 = 0
    K

    x = 5 × 10–3 = 5 mm



  1. A 10 mm diameter electrical conductor is covered by an insulation of 2 mm thickness. The conductivity of the insulation is 0.08 W/mK and the convection coefficient at the insulation surface is 10 W/m²K. Addition of further insulation of the same material will









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    rc = 8mm
    ∴ the heat lost increases to maximum and then decreases.

    Correct Option: C

    rc = 8mm
    ∴ the heat lost increases to maximum and then decreases.