Example (4-7): Air is supply to inlet nozzle with pressure and temperature at 210 kPa and 318 K where velocity is zero. The throat and exit cross-sectional areas for supersonic nozzle are 0.054 m2 and 0.12 m2 respectively. For isentropic flow with mass flow rate 14 kg/s, determine: r (a) The process on T-s diagram. (b) Flow properties at nozzle throat. (c) Flow properties at nozzle exit.
Example (4-7): Air is supply to inlet nozzle with pressure and temperature at 210 kPa and 318 K where velocity is zero. The throat and exit cross-sectional areas for supersonic nozzle are 0.054 m2 and 0.12 m2 respectively. For isentropic flow with mass flow rate 14 kg/s, determine: r (a) The process on T-s diagram. (b) Flow properties at nozzle throat. (c) Flow properties at nozzle exit.
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Transcribed Image Text:Example (4-7): Air is supply to inlet nozzle with pressure and
temperature at 210 kPa and 318 K where velocity is zero. The
throat and exit cross-sectional areas for supersonic nozzle are
0.054 m2 and 0.12 m2 respectively. For isentropic flow with
mass flow rate 14 kg/s, determine:
(a) The process on T-s diagram.
(b) Flow properties at nozzle throat.
(c) Flow properties at nozzle exit.
r (a)
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