Carbon dioxide enters an adiabatic nozzle steadily at 1 MPa, 518 oC, and mass flow rate of 5,322 kg/h and exits the system at 96
kPa and 421 m/s. Considering the nozzle having an inlet area of 37 cm2, calculate the inlet velocity in m/s
1 answer:
Answer:
The velocity at the nozzle at inlet
= 3584 
Explanation:
Pressure at inlet
= 1 ×
Pa
Temperature at inlet
= 518 ° c = 791 K
Mass flow rate =
= 88.7
Gas constant for carbon die oxide is R = 189 
Mass flow rate inside the nozzle is given by the formula =
×
×
⇒
= = 1 ×
Pa
⇒ R
= 791 × 189 = 149499 
⇒
= 0.0037 
Put all the above values in above formula we get,
⇒ 88.7 =
× 0.0037 × 
⇒
= 3584 
This is the velocity at the nozzle at inlet.
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