Air flows through the supersonic nozzle. The inlet conditions are 7 kPa and 4200C. The nozzle exit diameter is adjusted such that the exiting velocity is 700 m/s. calculate the exit temperature, the mass flux and the exit diameter. Assume adiabatic quasiequilibrium flow. Control surface V, = 400 m/s d, = 200 mm

Introduction to Chemical Engineering Thermodynamics
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Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
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Air flows through the supersonic nozzle. The inlet conditions are 7 kPa and 4200C. The nozzle exit
diameter is adjusted such that the exiting velocity is 700 m/s. calculate the exit temperature, the mass
flux and the exit diameter. Assume adiabatic quasiequilibrium flow.
Control
surface
V = 400 m/s
d, = 200 mm
Transcribed Image Text:Air flows through the supersonic nozzle. The inlet conditions are 7 kPa and 4200C. The nozzle exit diameter is adjusted such that the exiting velocity is 700 m/s. calculate the exit temperature, the mass flux and the exit diameter. Assume adiabatic quasiequilibrium flow. Control surface V = 400 m/s d, = 200 mm
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