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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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Basic <strong>Thermodynamics</strong>, <strong>Fluid</strong> <strong>Mechanics</strong>: Definitions <strong>of</strong> Efficiency 39<br />

FIG. 2.8. Relationship between isentropic (overall) efficiency, pressure ratio <strong>and</strong> small<br />

stage (polytropic) efficiency for a compressor (g = 1.4).<br />

The term polytropic used above arises in the context <strong>of</strong> a reversible compressor compressing<br />

a gas from the same initial state to the same final state as the irreversible adiabatic<br />

compressor but obeying the relation p n = constant. The index n is called the<br />

polytropic index. Since an increase in entropy occurs for the change <strong>of</strong> state in both<br />

compressors, for the reversible compressor this is possible only if there is a reversible<br />

heat transfer dQR = Tds. Proceeding further, it follows that the value <strong>of</strong> the index n must<br />

always exceed that <strong>of</strong> g. This is clear from the following argument. For the polytropic<br />

process,<br />

Using pv n = constant <strong>and</strong> C = R/(g - 1), after some manipulation the expression<br />

dQR = (g - n) / (g - 1) pd is derived. For a compression process d < 0 <strong>and</strong> dQ R > 0<br />

then n > g. For an expansion process d > 0, dQR < 0 <strong>and</strong> again n > g.<br />

EXAMPLE 2.1. An axial flow air compressor is designed to provide an overall totalto-total<br />

pressure ratio <strong>of</strong> 8 to 1. At inlet <strong>and</strong> outlet the stagnation temperatures are<br />

300K <strong>and</strong> 586.4K, respectively.<br />

Determine the overall total-to-total efficiency <strong>and</strong> the polytropic efficiency for the<br />

compressor. Assume that g for air is 1.4.<br />

Solution. From eqn. (2.28), substituting h = C pT, the efficiency can be written as

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