?_p`WlSLEnergy Conversion ... - HelpEngineering Software (c) 1996/&;)z4^F u|CONTEXT |CTXOMAP|FONT|SYSTEM|TOPIC|TTLBTREE#[+E[+jBjBU-#uhCh[+E[+mBjB |gB-#Qf[+nH[+FkBiBun-#z[+H[+tkBkBHe-#[+H[+pBFkBinuiU_PMingLiU_@PMingLiUbMyriad Condensed WebMyriad Webb-#us M [+$M[+pnBiB-#2v [+~M[+pB:hB-#C Av[+P[+ qBUgBt ITC ءQbCG Omega_CG TimesaITC Zapf Chancery_Clarendon-#Clar[+F[+rBjBnd9aCoro-#[+E[+prBIT-# Din[+G[+nBJiBU_nowidctlparcs16super#Engineering Softwarer%olb-b e Olv-#aD[+LH[+HnBSmB-#X[+`H[+vnf] 1=1 =j &9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.comD=j% >Energy Conversion 1.1 - Help&} Ȁ;\PS?$dIn\fvProgram DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPropertiesNj0 0<> Temperature - Pressurew4IC Vh? @ Enthalpy - PressureEntropy - Pressuren/? N^w Steam ApproximationsSaturated AreaJI2 40x Superheated Area^_? N> Power CyclesCarnotA2 4 BraytonI_3 6,n Power (Ideal)]m o p q   Power (Real)Propulsion (Ideal)Propulsion (Real)RankineOttok)B TR- - Power (Ideal)Power (Real)< Z/ .  Dieselg(? NP5 5 Power (Ideal)Power (Real)g*Z(= JT   MagnetohydrodynamicsFuel CellQN l B Power Cycle Components/ProcessesCompressionIsentropic (Ideal):(NM jt B B  Isentropic (Real)IsothermalCombustion@0 0  J Coal/OilXN> L4 J  GasExpansionJ0 0 04 XQ Isentropic (Ideal)I [  YQ ZQ   Isentropic (Real)IsothermalHeat TransferMixingj.0 > < H\ "& Compressible FlowVelocity of Sound_" = JD #& $& Mach NumberPropertiesB> 0 0$ | StagnationX 7 > L4 | %& StaticNozzleW ? N0B C IdealReal^!7 = JB && '& Normal ShockDiffuserW C ? N0㴑 㵑 IdealReal<  / . (& ThrustWC ? N0  IdealReal1  1  G 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  ?@< F Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Energy Conversion, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, steam approximations, analyzes power cycles, power cyclecomponents/processes and compressible flow.This software package should prove to be a good tool for those who areinvolved at variou?@ s levels with design, operation and management ofNB: B energy conversion systems. It should provide you with the opportunityto 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 Properties?@`Db a Temperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressureSteam ApproximationsSaturated Area (Temperature and Pressure Dependent)Superheated AreaPower CyclesCarnotBrayton (Power and Propulsion)RankineOttoDieselMagnetohydrodynamicsFuel CellPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionHeat TransferMixingCompressible FlowFNBEA P  Velocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:wI`DF. ,E Microsoft Windows 98, Windows 2000,Windows ME and Windows XP E(G, & 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.FG1 0K Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1(G/H1s/HqOGI9 @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+/HCI( Q ILK> 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:$CIpMB 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 andLKqOH ^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 constant1pMO19OqO9 @aءQEngineering SoftwareP.O. Box 1180OqO, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+O€( Q : BuءQ How to Use the ProgramIn each section, subsection of the Energy Conversion 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.1€1YЃ9 @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 7Ѓ2B 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) days from the date of purchase. If during thisCuP 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, thenm2- *ءQ Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1u@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+@T( Q L)- *>ءQ Suggestion/Evaluation FormT8 > 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]E4 8ءQ Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:=) "( ءQ Energy ConversionZE= JءQ Quality:Usefulness:Possible areas of improvement:Other suggestions:1J1kJ39 @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+J^( Q !3D 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 foll^ows:You may:- use one copy of the software on a single computer,- make one copy of the software for backup purposes, and^4 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 software11A9 @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 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 thatW.A) "\ءQ steam table calculations are not available.1r1rA[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+r( 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 constant11 X9 @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 B X9 @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 constant11 Xr9 @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 <r8 > 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 0 .1ءQ Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas. 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( Q & 8 >ءQ Steam Approximations: Saturated AreaThis subsection deals with steam approximations for the saturated area,steam table calculations are available for the saturated area only. In thiscase, steam approximations are either temperature or pressuredependent.Input Values:Saturated Steam Temperature and Pressure, Steam QualityOutput Values:Saturated Steam Physical Properties1Q=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( Q b,&6 :YءQ Steam Approximations: Superheated AreaThis subsection deals with steam approximations for the superheated area,steam table calculations are available for the superheated area only.Input Values:Superheated Steam Temperature and PressureOutput Values:Superheated Steam Physical Properties1Q1 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 CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).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 N 9 @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.1  1D @  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  ; 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\@D@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+@A( Q AC9 @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 RateAD. *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.1C#E1#E ID F9 @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+#E7F( Q 9 FpH< 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 powerq7F I* $ءQ output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1pHءQ 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.11c9 @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: MagnetohydrodynamicsThis subsection provides analysis of the Magnetohydrodynamics cycle.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet Stagnation Pressure,Velocity, Conductivity, Loading Parameter, Magnetic Field Strength,Channel LengthOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Outlet Static Temperature,Outlet Static Pressure, Outlet Mach Number, Outlet Stagnation/ ,ءQ Temperature, Outlet Stagnation Pressure, Enthalpy Extraction,Specific Work OutputAssumptions:Specific heat, velocity, conductivity, induced voltage field andmagnetic field strength are constant.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+1( Q ?/ , Power Cycles: Fuel CellThis subsection provides analysis of the Fuel Cell cycle.Input Values:Fuel, Fuel Inlet Temperature, Oxidant (O2) Inlet Temperature,Fuel Flow Rate, Product Outlet TemperatureOutput Values:mD1) "ءQ Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1?19 @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 .QءQ Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).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 e. ,ءQ Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.11o 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 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.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 : 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, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is 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 J_9 @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 compression11#5 _y 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 cy 5 . ,ءQ Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1 f 1$f  5 O 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+f z ( Q +O  ; 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!z  ) "BءQ Specific heat is not constant.1  1% A  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+ 4( Q  ]A; DءQ Power Cycle Components/Processes: Combustion: GasThis subsection provides analysis of the combustion process when gasis considered as the 4]A 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!4A) "BءQ Specific heat is not constant.1]AA1&A{CAB9 @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+AB( Q aB{C. ,ءQ Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1BC1'CZF{CD9 @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+CD( Q aDZF9 @ءQ Power Cycle Components/Processes: 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.1DF1(FVIZFtG9 @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+FG( Q ~tGVI9 @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.1GI1)ILVIpJ9 @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 |CpJL9 @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 expansion1JHL19*HLPOL1M9 @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+HL\M( Q 1MPO; DsءQ Power Cycle Components/Processes: Heat TransferThis subsection provides analysis of heat transfer.Input Values:Hot Working Fluid, Hot Working Fluid Mass Flow Rate, HotWorking Fluid Inlet Temperature, Hot Working Fluid Outlet Temperature,Cold Working Fluid, Cold Working Fluid Mass Flow Rate, ColdWorking Fluid Inlet TemperatureOutput Values:Cold Working Fluid Outlet TemperatureAssumptions:Ideal heat transfer -- no losses1\MO1.+OPPOv9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(30OvPO1) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+O( Q uvP: BءQ Power Cycle Components/Processes: MixingThis subsection provides analysis of mixing.Input Values:Inlet Working Fluids, Inlet Working Fluids Mass Flow Rate, InletWorking Fluids Temperature, Outlet Working Fluids, Outlet WorkingFluids Mass Flow RateOutput Values:Outlet Working Fluids Temperature -- Mixing TemperatureAssumptions:Ideal mixing -- no losses11,Pj9 @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 yKj. ,ءQ Compressible FlowThis section provides analysis of compressible flow.1?1S-?a(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+?S( Q (a8 >ءQ Compressible Flow: Velocity of SoundThis subsection provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1S1K.a{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 {8 >ءQ Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1݈1/݈ʉ< FcءQ Engineering 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 ʉ0 .ءQ Compressible Flow: PropertiesThis subsection provides analysis of stagnation and static properties inthe case of compressible flow.1108ʋ9 @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 C ʋ88 >ءQ Compressible Flow: Properties: StagnationThis subsection provides analysis of stagnation properties.Input Values:Working Fluid, Static Temperature, VelocityOutput Values:Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1i1|1i8R9 @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+i}( Q 7R8 >ءQ Compressible Flow: Properties: StaticThis subsection provides analysis of static properties.Input Values:Working Fluid, Stagnation Temperature, VelocityOutput Values:Static Temperature, Static PressureAssumptions:Specific heat is constant1} 1e2  < FcءQ Engineering 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 zL. ,ءQ Compressible Flow: NozzleThis subsection provides analysis of nozzle.1$130< FcءQ Engineering 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 I08 >#ءQ Compressible Flow: Nozzle (Ideal)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1a14a0N< FcءQ Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ay( Q `N: BءQ Compressible Flow: Nozzle (Real)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, Ideal Velocity,Nozzle EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, StaticTemperature, Mach Number, VelocityAssumptions:Specific heat is constant1yD1L5D_-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+DX( Q -_< FءQ Compressible Flow: Normal ShockThis subsection provides analysis of normal shock.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet StagnationPressure, Inlet VelocityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach NumberOutlet Stagnation Temperature, Outlet Stagnation Pressure, OutletVelocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1X16&_}< FcءQ Engineering 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 ~P}&. ,ءQ Compressible Flow: DiffuserThis subsection provides analysis of diffuser.1W17W&@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+Wk( Q M@8 >+ءQ Compressible Flow: Diffuser (Ideal)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1k189 @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  G: BءQ Compressible Flow: Diffuser (Real)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, Velocity,Diffuser EfficiencyOutput Values:Mach Number, Ideal Stagnation Temperature, Stagnation Pressure,Stagnation TemperatureAssumptions:Specific heat is constant1 19P< FcءQ Engineering 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 zLP. ,ءQ Compressible Flow: ThrustThis subsection provides analysis of thrust.11:Pj9 @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 Hj8 >ءQ Compressible Flow: Thrust (Ideal)This subsection provides analysis of thrust.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Stagnation Temperature,Stagnation Pressure, Velocity, Ambient PressureOutput Values:Static Temperature, Static Pressure, Mach Number, ThrustAssumptions:Specific heat is constant1F1;F, /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+FZ( Q /, : B1ءQ Compressible Flow: Thrust (Real)This subsection provides analysis of thrust.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Stagnation Temperature,Stagnation Pressure, Ideal Velocity, Ambient Pressure, Thrust EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, Thrust,Static Temperature, Velocity, Mach NumberAssumptions:Specific heat is constant1Z1<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 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