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By Kenneth C. Weston

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The mass-flow rate is determined by the physical requirement that the feedwater entering the FWH at state 5 increase in temperature to T6 through absorption of the heat released by the condensing extraction steam. This is accomplished by applying the steady-flow First Law of Thermodynamics, using appropriate mass fractions, to the insulated open FWH: q = 0 = (1)h6 – m1h2 – (1 – m1 )h5 + 0 [Btu/lbm | kJ/kg] Every term in this equation has dimensions of energy per unit throttle mass, thus referring all energy terms to the mass-flow rate at the throttle of the high-pressure turbine.

Thermodynamics. New York: McGrawHill, 1989. 30 4. Faires, Virgil Moring, Thermodynamics, 5th ed. New York: Macmillan, 1970. 5. , Engineering Thermodynamics. Minneapolis: West, 1977. 6. , Fundamentals of Gas Turbines. New York: Wiley, 1984 7. Wilson, David Gordon, The Design of High Efficiency Turbomachinery and Gas Turbines. Boston: MIT Press, 1984. 8. , Modern Compressible Flow. New York: McGraw-Hill, 1982. 9. , Introduction to Flight. New York: McGraw-Hill, 1978. 10. Chapman, Alan J. , Introductory Gas Dynamics.

Heat-Power Engineering. Wiley, 1926. 2. NewYork: Oxford University Press, 1965 3. Cummins, C. , Internal Fire, rev. ed. : Society of Automotive Engineers, 1989. 4. Tann, Jennifer, The Selected Papers of Boulton and Watt. Boston: MIT Press, 1981. 5. Carnot, Sadi, Reflexions Sur la Puissance Motrice de Feu. Paris: Bachelor,1824. 6. Potter, J. ” ASME Paper presented at the Gas Turbine Forum Dinner, ASME Annual Meeting, New York, Nov. 27, 1972. 7. Grosser, Morton, Diesel: The Man and the Machine.