Air at 6.9 bar,260 oC is throttled to 5.5bar before 10. nozzle to 1.1 bar. Assuming that the air flow reversibly in steady flow through the nozzle, and that no heat is rejected, calculate the velocity of the air at exit from the nozzle when the inlet velocity is 100m/s. (637m/s) miring chamber where it mixes with 540kg/hr 10°C

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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(270 C,5.1
Air at 6.9 bar 260 oC is throttled to 5.5bar before expanding through a
nozzle to 1.1 bar. Assuming that the air flow reversibly in steady flow through the
nozzle, and that no heat is rejected, calculate the velocity of the air at exit from the
(637m/s)
here it mixes with 540kg/hr
10.
nozzle when the inlet velocity is 100m/s.
10°Can
miring chan
Transcribed Image Text:(270 C,5.1 Air at 6.9 bar 260 oC is throttled to 5.5bar before expanding through a nozzle to 1.1 bar. Assuming that the air flow reversibly in steady flow through the nozzle, and that no heat is rejected, calculate the velocity of the air at exit from the (637m/s) here it mixes with 540kg/hr 10. nozzle when the inlet velocity is 100m/s. 10°Can miring chan
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