Question

Briefly explain why it is beneficial to provide compressor applications. Also, what are the benefits of performing combustor applications. in gas turbine reheat in these ot gases are generated in a combustion chamber at a stagnation pressure of 10 Mpa. These gases are expanded through a converging/diverging nozzle. It is observed that a normal shock is standing in the diverging section of the nozzle at the location where the cross sectional area is approximately twice that of the throat. Assuming for these gases (k-1.4), estimate the static pressure just downstream of this normal shock sitting in the diverging section of the nozzle 8. Why are equations of state typically written in terms of temperature, pressure and volume? 8

Answer 1

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