Page 55 - Fluid Mechanics and Thermodynamics of Turbomachinery
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36 Fluid Mechanics, Thermodynamics of Turbomachinery
                            From the relation Tds D dh  vdp, for a constant pressure process .∂h/∂s/ p 1  D T.
                          This means that the higher the fluid temperature the greater is the slope of the
                          constant pressure lines on the Mollier diagram. For a gas where h is a function
                          of T, constant pressure lines diverge and the slope of the line p 2 is greater than
                          the slope of line p 1 at the same value of entropy. At equal values of T, constant
                          pressure lines are of equal slope as indicated in Figure 2.6. For the special case
                          of a perfect gas (where C p is constant), C p .dT/ds/ D T for a constant pressure
                          process. Integrating this expression results in the equation for a constant pressure
                          line, s D C p log T C constant.
                            Returning now to the more general case, since
                                                                     h 1 /,
                              υW Df.h x   h 1 / C .h y  h x / CÐ Ð Ðg D .h 2
                          then

                                                                  h 1 /.
                                p D [.h xs  h 1 / C .h ys  h x / C ÐÐÐ]/.h 2
                          The adiabatic efficiency of the whole compression process is
                                                 h 1 /.
                                c D .h 2s  h 1 //.h 2
                            Because of the divergence of the constant pressure lines
                                                                h 1 /,
                              f.h xs  h 1 / C .h ys  h x / C ÐÐÐg >.h 2s
                          i.e.

                              υW min >W min .
                          Therefore,

                                p >  c .
                          Thus, for a compression process the isentropic efficiency of the machine is less than
                          the small stage efficiency, the difference being dependent upon the divergence of
                          the constant pressure lines. Although the foregoing discussion has been in terms of
                          static states it can be regarded as applying to stagnation states if the inlet and outlet
                          kinetic energies from each stage are equal.

                          Small stage efficiency for a perfect gas

                            An explicit relation can be readily derived for a perfect gas (C p is constant)
                          between small stage efficiency, the overall isentropic efficiency and pressure ratio.
                          The analysis is for the limiting case of an infinitesimal compressor stage in which
                          the incremental change in pressure is dp as indicated in Figure 2.7. For the actual
                          process the incremental enthalpy rise is dh and the corresponding ideal enthalpy
                          rise is dh is .
                            The polytropic efficiency for the small stage is
                                           vdp
                                   dh is
                                p D    D                                                  (2.31)
                                    dh   C p dT’
                                                                   vdp.
                          since for an isentropic process Tds D 0 D dh is
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