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
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The exit area of the nozzle in cm² is
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- 90.1
- 56.3
- 4.4
- 12.9
Correct Option: D
From continuity equation, we get
ρ1 A1 V1 = ρ2 A2 V2
∴ | × A1V1 = | × A2V2 | ||
RT1 | RT2 |
⇒ A2 = | × | × A1 | × | × 80 = 12.9 cm² | ||||
P2T1 | V2 | 500 × 100 | 180 |