ThermodynamicsThis edition of "Thermodynamics" continues the tradition of providing a fundamentally sound, well-written, technically accurate text. This new edition addresses the needs of today's marketplace through the following enhancements: a greater emphasis on thermoeconomics and current real world applications, more design problems, more real world and visual problems, a re-vamped design and a stronger pedagogical program. The book will also be available with or without EES (Engineering Equation Solver) Problems Disk. Professor Donald E. Richards of Rose-Hulman Institute of Technology has been added as a co-author for this edition. |
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Page 233
... energy changes are frequently negligible . For gas flow the kinetic - energy change could become relatively large when heat transfer is significant or cross ... energy balance for the control CHAPTER 233 CONTROL - VOLUME ENERGY ANALYSIS.
... energy changes are frequently negligible . For gas flow the kinetic - energy change could become relatively large when heat transfer is significant or cross ... energy balance for the control CHAPTER 233 CONTROL - VOLUME ENERGY ANALYSIS.
Page 449
... energy changes across a turbine are negligible , the energy balance given by Eq . [ 8-15 ] reduces to hh2 . In this case the adiabatic turbine efficiency becomes - ητ = h1 - h2a h1 - h2s h P1 h1 - h2s h1 - ha 2a 12s P2 ( turbine with ...
... energy changes across a turbine are negligible , the energy balance given by Eq . [ 8-15 ] reduces to hh2 . In this case the adiabatic turbine efficiency becomes - ητ = h1 - h2a h1 - h2s h P1 h1 - h2s h1 - ha 2a 12s P2 ( turbine with ...
Page 730
... energy balance is Q + W = - Ntuel Σnihi - Σnihi thi - Enchi prod reac = Nfuel [ hprod - hreac ] where n1 = N¡ / Nfuel and hprod and reac are the enthalpy per mole of fuel of the products and the reactants , respectively . Typically ...
... energy balance is Q + W = - Ntuel Σnihi - Σnihi thi - Enchi prod reac = Nfuel [ hprod - hreac ] where n1 = N¡ / Nfuel and hprod and reac are the enthalpy per mole of fuel of the products and the reactants , respectively . Typically ...
Contents
BASIC CONCEPTS AND DEFINITIONS | 1 |
THE FIRST LAW OF THERMODYNAMICS | 36 |
PROPERTIES OF A PURE SIMPLE COMPRESSIBLE | 95 |
Copyright | |
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Common terms and phrases
adiabatic efficiency adiabatic process air-fuel ratio air-standard analysis bars Brayton cycle Btu/lbm Calculate Carnot Celsius closed system combustion compression condenser constant pressure control volume cooling Determine dry air energy balance enthalpy entropy balance entropy change entropy production equilibrium evaluate exit expansion feedwater heater final temperature Find fluid ft/s fuel gas-turbine gases given h₁ h₂ heat engine heat exchanger heat pump heat transfer heat-transfer heater ideal ideal-gas inHg initial inlet input internal energy internally reversible irreversible isentropic isothermal kelvins kilojoules kJ/K kJ/kg kJ/kg.K kJ/kmol kJ/min m³/kg mass flow rate mixture mole nozzle output piston piston-cylinder device power cycle pressure ratio Prob psia Rankine cycle reaction refrigerant 134a Schematic and data second law shown in Fig specific heats specific volume steady-flow steady-state steam superheat T₁ thermal efficiency thermal reservoir thermodynamic turbine velocity water vapor Wnet