Math, asked by pranay2091, 4 months ago

A jet engine turbine recive gases at 7.5 bar and 900 degree C and 170 m/s. it discharges the gases at 2.5 bar 650 degree C and 340m/s. find the work output of the turbine.take c1= 1.3 kj/kg k.​

Answers

Answered by Anonymous
0

Step-by-step explanation:

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Answered by mariyamkmariyam382
0

Step-by-step explanation:

Air is discharged from a C - D nozzle. ...

A converging, nozzle operating with air and inlet conditions of P = 4 Kg/cm2, T0 = 450oC and T = 400oC is expected to have an exit static pressure of 2.5 Kgf/cm2 under ideal conditions. ...

An aircraft flies at a speed of 520 kmph at an altitude of 8000 m.

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