Thermodynamics Miscellaneous


Direction: Air enters an adiabatic nozzle at 300 kPa, 500 K with a velocity of 10 m/s. It leaves the nozzle at 100 kPa with a velocity of 180 m/s. The inlet area is 80 cm². The specific heat of air c is 1008 J/kgK

  1. The exit temperature of the air is









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    h1 =
    1
    = h2 +
    2
    22

    2 - V²1
    = h1 - h2 = Cρ(T1 - T2)
    2

    &There4;
    180² - 10²
    = 1008 × (500 - T2)
    2

    ⇒ T2 = 484K

    Correct Option: C

    h1 =
    1
    = h2 +
    2
    22

    2 - V²1
    = h1 - h2 = Cρ(T1 - T2)
    2

    &There4;
    180² - 10²
    = 1008 × (500 - T2)
    2

    ⇒ T2 = 484K


  1. Steam enters a well insulated turbine and expands isentropically throughout. At an intermediate pressure, 20 percent of the mass is extracted for process heating and the remaining steam expands isentropically to 9 kPa.
    Inlet to turbine: P = 14 MPa, T = 560°C,
    h = 3486 kJ/kg, s = 6.6 kJ/(kgK)
    Intermediate stage: h = 276 kJ/kg
    Exit of turbine: P = 9 kPa, hf = 174 kJ/kg,
    hg = 2574 kJ/kg, sf = 0.6 kJ/(kgK), sg = 8.1 kJ/(kgK)
    If the flow rate of steam entering the turbine is 100 kg/s, then the work output (in MW) is____.









  1. View Hint View Answer Discuss in Forum

    h1 = 3486 kJ/kg
    h2 = 2776 kJ/kg
    s1 = s3 = 6.6
    6.6 = .6 + x(0.1 – .6)
    x = 0.8

    = 2094 kJ/kg
    w = (3486 – 2776) + .8 (2776 – 2094)
    = 1255.6 kJ/kg = 125.56 MW

    Correct Option: B

    h1 = 3486 kJ/kg
    h2 = 2776 kJ/kg
    s1 = s3 = 6.6
    6.6 = .6 + x(0.1 – .6)
    x = 0.8

    = 2094 kJ/kg
    w = (3486 – 2776) + .8 (2776 – 2094)
    = 1255.6 kJ/kg = 125.56 MW



  1. The mass flow rate of air through the nozzle in kg/s is









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    Mass flow rate, m = ρQ
    where, Q = A2 V2
    But V2 = √2CP(T1 - T2)
    = √2 × 1.005 × (400 - 239.5) = 568 m/s
    ∴ m = 0.727 × 0.005 × 568 = 2.06 kg/s

    Correct Option: D

    Mass flow rate, m = ρQ
    where, Q = A2 V2
    But V2 = √2CP(T1 - T2)
    = √2 × 1.005 × (400 - 239.5) = 568 m/s
    ∴ m = 0.727 × 0.005 × 568 = 2.06 kg/s


  1. The thermal efficiency of an air-standard Brayton cycle in terms of pressure ratio rρ and γ(= cρ /cv) is given by









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    Thermal efficiency of air standard efficiency = 1 –
    1
    (rρ)γ-1/γ

    Correct Option: D

    Thermal efficiency of air standard efficiency = 1 –
    1
    (rρ)γ-1/γ



  1. The exit area of the nozzle in cm² is









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    From continuity equation, we get
    ρ1 A1 V1 = ρ2 A2 V2

    P1
    × A1V1 =
    P2
    × A2V2
    RT1RT2

    ⇒ A2 =
    P1T2
    ×
    V2
    × A1
    300 × 484
    ×
    10
    × 80 = 12.9 cm²
    P2T1V2500 × 100180

    Correct Option: D

    From continuity equation, we get
    ρ1 A1 V1 = ρ2 A2 V2

    P1
    × A1V1 =
    P2
    × A2V2
    RT1RT2

    ⇒ A2 =
    P1T2
    ×
    V2
    × A1
    300 × 484
    ×
    10
    × 80 = 12.9 cm²
    P2T1V2500 × 100180