It is required to expand 3 kg/s of air from stagnation conditions of 200kPa, 500K through a convergent-divergent nozzle to give an exit Mach No. of 2.5. Determine: (i) throat area (ii) exit pressure...

It is required to expand 3 kg/s of air from stagnation conditions of 200kPa, 500K through<br>a convergent-divergent nozzle to give an exit Mach No. of 2.5.<br>Determine:<br>(i) throat area<br>(ii) exit pressure<br>(iii) exit temperature<br>(iv) exit velocity<br>(v) exit area<br>Ans: 0.0083m², 11.7kPa, -51°C, 747m/s, 0.0219m?<br>

Extracted text: It is required to expand 3 kg/s of air from stagnation conditions of 200kPa, 500K through a convergent-divergent nozzle to give an exit Mach No. of 2.5. Determine: (i) throat area (ii) exit pressure (iii) exit temperature (iv) exit velocity (v) exit area Ans: 0.0083m², 11.7kPa, -51°C, 747m/s, 0.0219m?

Jun 11, 2022

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It is required to expand 3 kg/s of air from stagnation conditions of 200kPa, 500K through a convergent-divergent nozzle to give an exit Mach No. of 2.5. Determine: (i) throat area (ii) exit pressure...

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