?_ue\l>L"Power Systems Analysis ... - HelpEngineering Software (c) 1996/&;)z4^F u|CONTEXT|CTXOMAP|FONT|SYSTEM|TOPIC|TTLBTREEZZ  mpm T T nowidctlparcs16super#Engineering Software%# SimSn-#[+E[+tkBHe-#[+E[+kBFkBin-#[+E[+:nBtkBB-#[+Q[+pB}eBMy-#eb[+R[+rBfBb usءQbAlbertus Extra BoldbITC Avant Garde GotbITC Avant Garde Got_ITC Bookman Light_ITC Bookman DemibCG Omega_CG TimesaITC Zapf Chancery_Clar-# [+M[+DoBjBCl-#n Ex[+P[+qB9 Temperature - Pressurew4NC Vh? @ Enthalpy - PressureEntropy - Pressure^? N> Power CyclesCarnotAN2 4 BraytonI63 6,n Power (Ideal)]m o p q   Power (Real)Propulsion (Ideal)Propulsion (Real)RankineOttok)6kB TR- - Power (Ideal)Power (Real)< / .  Dieselxkl 5 5  B Power (Ideal)Power (Real)Power Cycle Components/ProcessesCompressionIsentropic (Ideal):M jt B B  Isentropic (Real)IsothermalCombustion@R0 0  J Coal/OilX> L4 J  GasExpansionJR0 04 XQ Isentropic (Ideal)i*]? NT YQ ZQ Isentropic (Real)Isothermal11 B]w 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ ( Q ;w < F Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power Systems Analysis, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, analyzes power cycles and power cycle components/processes.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunity @ N to more quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outmore about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (301) 540-3605.Thermodynamic and Transport PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureU U x Entropy and PressurePower CyclesCarnotBrayton (Power and Propulsion)RankineOttoDieselPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:wI @. ,E Microsoft Windows 98, Windows 2000,Windows M @]E and Windows XP +A, & Distributed on CD ROMFree Technical and Product Support30 Day Money Back GuaranteeTrademarks:All product names, company names andservice marks are trademarks or registered trademarks of theirrespective companies. @B1 0K Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1+A2B1s2BtIBC9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+2BFC( Q COE> JءQ Claim SheetEngineering Software products allow quick and reliablecalculation of thermodynamic and transport properties ofgaseous, liquid and solid species, contain coefficients forthe calculation of physical properties, steam approximationsfor both saturated and superheated areas, analyze powercycles, power cycle components/processes andcompressible flow.The aforementioned engineering calculations are valid underthe following assumptions:$FCsGB RءQ Thermodynamic and Transport PropertiesSingle species considerationIdeal gas approach is used (pv=RT)Specific heat is not constantCoefficients describing thermodynamic and transport propertieswere obtained from the NASA Glenn Research Center at LewisField in Center in Cleveland, OH -- such coefficients conform withthe standard reference temperature of 298.15 K (77 F) and theJANAF tablesPower CyclesSingle species consideration -- fuel mass flow rate ignored andOEtIH ^sءQ its impact on the properties of the working fluidBasic equations hold (continuity, momentum and energyequations)Specific heat is constantPower Cycle Components/ProcessesSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constantCompressible FlowSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constant1sGI1=ILtIJ9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+IJ( Q JL: B}ءQ How to Use the ProgramIn each section, subsection of the Power Systems Aalysis program, theuser needs to change one or more input values in order to calculate anew case. Input values are in boxes with white background and can bechanged by clicking on each individual box or even by using the arrowkeys and changing the current value. Output values cannot be modified,changed by the user and they are in boxes with black background.1JL1YLLM9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+LM( Q 7M9B RءQ Limited WarrantyThis software package is sold AS IS, without warranty as to itsperformance. The entire risk (as to) the quality and of the performanceof this computer software program is assumed by the user.However, to the original purchaser only, Engineering Software warrantsthe medium on which the program is recorded to be free from defects inmaterials and faulty workmanship under normal use and service for aperiod of thirty (30) daysM9L from the date of purchase. If during thisCM|P nءQ period a defect on the medium should occur, the medium may bereturned to Engineering Software or to an authorized EngineeringSoftware distributor, and Engineering Software will replace themedium without charge to you. Your sole and exclusive remedy in theevent of a defect is expressly limited to replacement of the medium asprovided above.If the failure of the medium, in the judgment of Engineering Softwareresulted from accident, abuse, or misapplication of the medium, thenm9- *ءQ Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1|G1G%09 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+G[( Q L0- *>ءQ Suggestion/Evaluation Form[8 > ءQ Please FAX or Mail This Suggestion/Evaluation Form To:Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com]L4 8ءQ Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:B) "2 ءQ Power Systems AnalysisZL%= JءQ Quality:Usefulness:Possible areas of improvement:Other suggestions:1V1kV%?9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Vj( Q !?D VءQ License AgreementThis software is the property of Engineering Software and is protectedby federal copyright law. While Engineering Software continues to ownthe software, you will have certain rights to use the software afteryour acceptance of this license. Your rights and obligations withrespect to the use of this software are as follows:You may:- use one copy of the software on a single computer,- make one copy of the software for backup purposes, andj4 6ءQ - use the software on a network, provided that you have a licensed copy of the software for each computer that can access the software over the networkYou may not:- copy the documentation which accompanies the software,- sublicense, rent or lease any portion of the software, and- reverse engineer, decompile, disassemble, modify, translate, make any attempt to discover the source code of the software, or create derivative works from the software11c9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ս( Q  6 :ءQ PropertiesThis section provides physical properties of available species forassigned two state values such as: temperature and pressure,enthalpy and pressure, and entropy and pressure. Physical propertiesare given in both U.S. customary and International units.Note: Physical properties for H2O(S), H2O(L) and H2O(G) areavailable. The accuracy of the available H2O properties is only goodfor the purpose of combustion calculation. Therefore, this indicates thatՍ W.Սc) "\ءQ steam table calculations are not available.1 1c}9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q K}9 @%ءQ Properties: Temperature - PressureThis subsection provides physical properties of the selected species forassigned temperature and pressure.Input Values:Species, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1$1 $z 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+$8( Q B  z9 @ءQ Properties: Enthalpy - PressureThis subsection provides physical properties of the selected species forassigned enthalpy and pressure.Input Values:Species, Enthalpy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant181 z9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q <8 > ءQ Properties: Entropy - PressureThis subsection provides physical properties of the selected species forassigned entropy and pressure.Input Values:Species Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1,1 ,9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+,@( Q s/ .ءQ Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto and Diesel).1@1 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+'( Q N9 @ءQ Power Cycles: CarnotThis subsection provides analysis of the Carnot cycle.Input Values:Heat Addition Temperature, Heat Rejection TemperatureOutput Values:Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Heat addition and rejectionoccur at constant temperature. Specific heat is constant.1'1 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q 0 .ءQ Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.119 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ ( Q "; DءQ Power Cycles: Brayton: Power (Ideal)This subsection provides analysis of the Brayton cycle for the powergeneration application.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer. * $ءQ Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1"1\'9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q $9 @ءQ Power Cycles: Brayton: Power (Real)This subsection provides analysis of the Brayton cycle for the powergeneration application.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat Rate'. *ءQ Assumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1$X1X@ 'A9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Xl( Q 9A < FءQ Power Cycles: Brayton: Propulsion (Ideal)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine powerql@ * $ءQ output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1 q 1oq @ Z 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+q  ( Q I Z < FءQ Power Cycles: Brayton: Propulsion (Real)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer. + $mءQ Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.11NB@9 @a@ءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+A( Q [@B: BءQ Power Cycles: RankineThis subsection provides analysis of the Rankine cycle.Input Values:Turbine Inlet Conditions (Temperature and Pressure), Steam Mass FlowRate, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion and heattransfer.1AB1BlDBC9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+BC( QdClD. ,ءQ Power Cycles: OttoThis subsection provides analysis of the Otto cycle for power applications.1CD1DNHlDE9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+DE( Q3EG9 @ءQ Power Cycles: Otto (Ideal)This subsection provides analysis of the Otto cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Revolutions, Fuel HHV,Number of Cylinders, Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel Consumptionj?ENH+ &~ءQ Assumptions:Specific heat is constant. Four stroke engine.1GH1?HLNHhI9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+HI( Q hIK9 @ءQ Power Cycles: Otto (Real)This subsection provides analysis of the Otto cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Revolutions, Fuel HHV,Number of Cylinders, Cylinder Stroke, Stroke to Diameter Ratio,Compression Isentropic Efficiency, Combustion Efficiency,Expansion Isentropic EfficiencyOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,IL. *ءQ Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1KL1LhNLM9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+LM( QhMhN. ,ءQ Power Cycles: DieselThis subsection provides analysis of the Diesel cycle for power applications.1MN1NkhNO9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+NO( Q :O9 @ءQ Power Cycles: Diesel (IdOhNeal)This subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Revolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelxLOk, (ءQ ConsumptionAssumptions:Specific heat is constant. Four stroke engine.11Sk9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q 8 >ءQ Power Cycles: Diesel (Real)This subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Revolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter Ratio, Compression Isentropic Efficiency,Combustion Efficiency, Expansion Isentropic EfficiencyOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,/ ,ءQ Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelConsumptionAssumptions:Specific heat is constant. Four stroke engine.11Ĉ؇9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q ؇Ĉ0 .#ءQ Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).11Ĉމ9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ ( Q eމ. ,ءQ Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1 ͊1͊9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+͊( Q f9 @ءQ Power Cycle Components/Processes: Compression: Isentropic (Ideal)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.11M9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ŏ( Q : BءQ Power Cycle Components/Processes: Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, CompressorIseŎntropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1Ŏ1Z9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q JZ9 @ءQ Power Cycle Components/Processes: Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression110Zt9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q ct0. ,ءQ Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1a1a0J9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+au( Q +J; DءQ Power Cycle Components/Processes: Combustion: Coal/OilThis subsection provides analysis of the combustion process when coalor oil are considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!u) "BءQ Specific heat is not constant.11 9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+/( Q L; DءQ Power Cycle Components/Processes: Combustion: GasThis subsection provides analysis of the combustion process when gasis considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!/) "BءQ Specific heat is not constant.1L1!j9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q aj. ,ءQ Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.11"Uj9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q aU9 @ءQ Power Cycle Components/UjProcesses: Expansion: Isentropic (Ideal)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.11#QUo9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q ~oQ9 @ءQ Power Cycle Components/Processes: Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.11$Qk9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+( Q |Ck9 @ءQ Power Cycle Components/Processs: Expansion: IsothermalThis subsection provides analysis of isothermal expansion.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal expansion11%443HelvG"F ^ &G"HTms RmnRP&GX^ &Symbol^ &G"F$CourierV$Times New Roman&Arial-@^ &G'FMS Serif*-@^ &GMS Sans Serif+~ Times&t#&Helveticaى^F&GSystem&*ߎF Courier NewF&G)FRomanG*@t/^&tScript&G+F&Modern&G+F&MarlettGZRP&GXArial CEG)RP\<Arial CYRF &9u'~;Arial Greek+F^_Arial TURWVv FVArial Baltic>Courier New CEuvCourier New CYRCourier New Greek^_Courier New TURPCourier New BalticLucida ConsoleދLucida Sans UnicodeTimes New Roman CEGTimes New Roman CYRTimes New Roman GreTimes New Roman TURTimes New Roman BalWingdings}uVerdanaFNF Arial BlackFFComic 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