revata:
The principle that pressure drop is proportional to the square of the flow only holds for incompressible fluids. In the case of a steam turbine, it generates power by virtue of a transfer of kinetic energy from the gas molecules to the rotating blades, and the tubine geometry is carefully designed to maximize the efficiency of this transfer . This is maximized when the rfelative velocity of the blade to gas bulk flow is about 50% of soundspeed.
bottom line is that for a constant speed turbine with constant area Ai at blade row "i", the relationship between flow and pressure is :
W= KAiPi/ SQRT(Ti+460)
W= flow , lb/hr
K= proportional constant
Ai= flree flow area between blades at row i, ft2
Pi= pressure entering row i, psia
T= temperature entering row i, F
each succeeding row has a larger area A, so the pressure ration between any set of rows is a constant ratio ( aproximately), and this ratio slightly varies only as the ratio of specific heats Cp/Cv changes over large changes in process conditions.
regarding a new vs old turbine, as the turbine ages, the clearance between blades increases due to solid partical exfoiliation erosion, so A increases at the first few rows of blades. The area A decreases over time at teh middle of an old turbine due to build up of deposits.