at a point upstream of the throat in a converging-diverging nozzle the velocity temperature and pressure are 192 m/s , 41C°,282 kpa , respectively if the nozzle is operating at its design condition and has an exit area of 0.03 m^2 and discharge to the atmosphere with a pressure of 110 kpa determine the mass flow rate and the the nozzle throat area

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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Gas dynamics
at a point upstream of the throat in
a converging-diverging nozzle the
velocity temperature and pressure are
192 m/s , 41C° , 282 kpa , respectively.
if the nozzle is operating at its design
condition and has an exit area of 0.03
m^2 and discharge to the atmosphere
with a pressure of 110 kpa determine
the mass flow rate and the the nozzle
throat area
Transcribed Image Text:at a point upstream of the throat in a converging-diverging nozzle the velocity temperature and pressure are 192 m/s , 41C° , 282 kpa , respectively. if the nozzle is operating at its design condition and has an exit area of 0.03 m^2 and discharge to the atmosphere with a pressure of 110 kpa determine the mass flow rate and the the nozzle throat area
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