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 nozzle when the inlet velocity is 100m/s.
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 nozzle when the inlet velocity is 100m/s.
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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
nozzle when the inlet velocity is 100m/s.
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