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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 area of the nozzle in cm² is
    1. 90.1
    2. 56.3
    3. 4.4
    4. 12.9
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



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