?_(ofleL,Power and Propulsion Systems ... - TutorialEngineering Software (c) 1996/&;)z460&^F |CONTEXTp |CTXOMAP6|FONT|SYSTEM|TOPIC|TTLBTREEA-#[+O[+xnB!eBV a^K[+nBnxfB ءQUNSimSunU@NSimSunVSimHeiV@SimHeiUMingLiUU@MingLiU_PMingLiU_@PMingLiUbMyriad Condens We-#ad W [+L[+N l B Power Cycle Components/ProcessesCompressionIsentropic (Ideal)h62 4l <% Running - Compression: Isentropic (Ideal)I>0 02 B Isentropic (Real)g5V2 4j <% Running - Compression: Isentropic (Real)B0 0$ B Isothermal`.V2 4\ =% Running - Compression: Isothermal@8 / ."  Combustion@x 0 0  J Coal/Oil]+8 2 4V Ws% Running - Combustion: Coal/Oil; x  0 0 J GasX& h 2 4L s% Running - Combustion: Gas? / .   ExpansionJh 0 04 XQ Isentropic (Ideal)f4 W 2 4h ꩂ% Running - Expansion: Isentropic (Ideal)I 0 02 YQ Isentropic (Real)e3W  2 4f % Running - Expansion: Isentropic (Real)B G 0 0$ ZQ Isothermal^, 2 4X @% Running - Expansion: IsothermalEG . ,.Compressible FlowA + / .$ #& Mach NumberQ | 1 2@ h Running - Mach Number< + / . %& NozzleL| 1 26 Yh Running - NozzleB F/ .& && Normal ShockR!1 2B h Running - Normal Shock>F/ . '& DiffuserN$1 2: h Running - Diffuser< `/ . (& ThrustL$1 26 h Running - Thrust1`1 H@9 @aء@QEngineering 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< F  Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power and Propulsion Systems Analysis, that quickly andreliably analyzes power cycles, power cycle components/processes andcompressible flow.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@EG \    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.Power CyclesCarnotBrayton (Power and Propulsion)RankinePower Cycle Components/ProcessesaCrFK d-  CompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowMach NumberNozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:wIEF. ,EMicrosoft Windows 98, Windows 2000,Windows ME and Windows XP rFG, &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.FH1 0K Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1GH1sHIHI9 @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+HJ( Q IL> 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:$JءQSuggestion/Evaluation Form58 > 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]&4 8ءQName:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:Q(w) "P ءQ Power and Propulsion Systems AnalysisZ&= JءQQuality:Usefulness:Possible areas of improvement:Other suggestions:1w?1k?(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 !(D VءQ  License AgreementThis software is the property of Engineering Software and is protectedby federal Scopyright 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, andS4 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 software11^9 @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 e^/ .ءQPower CyclesThis section provides analysis of a few power cycles (Carnot, Brayton andRankine).11*^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 Nx*9 @ءQPower 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[1N [x*D9 @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+[o( Q Dx= HءQRunning - Power Cycles: CarnotSTEP 1Enter the desired heat addition temperature value or go with the defaulttemperature value.STEP 2Enter the desired heat rejection temperature value or go with the defaulttemperature value.STEP 3Click on the Calculate button to start the calculation of the Carnot cycleoutput values for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1o1 vx9 @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 v0 .ءQPower Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.11 v9 @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 ; DءQPower 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 vTemperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.* $ءQFuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.11i 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 @ ? LءQRunning - Power Cycles: Brayton: Power (Ideal)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the default9 @WءQturbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1  1\ K  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  H 9 @ءQPower 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 Rate4K . *ءQAssumptions: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.1H | 1| CBK e 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 =e ? LءQRunning - Power Cycles: Brayton: Power (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultA A< F ءQturbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the compressor isentropic effiAK ciency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor)CB2 2ءQefficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go back to the Main menu.1AtB1tB\FCB]C9 @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+tBC( Q 9]CE< FءQPower 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 powerqC\F* $ءQoutput. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1EF1mFK\FvG9 @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 DvGI? L ءQRunning - Power Cycles: Brayton: Propulsion (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3 Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultGK9 @WءQturbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1IK1wKDKL9 @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+KM( Q I LWO< FءQPower 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.MD+ $mءQFuel mass flow rate is ignored when calculating the gas turbine poweroutput. Ambient pressure is equal to compressor inlet WODKpressure.No pressure loss. Specific heat is constant.1WOu1u6Db< 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+u( Q Bbσ? LءQRunning - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultA< F ءQturbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the compressor isentropic efficiency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor&σ61 0ءQefficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1g1g6P9 @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 [P: BءQPower 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.1{A1A*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+AU( Q *d< FءQRunning - Power Cycles: RankineSTEP 1Select the desired steam turbine inlet conditions (temperature andpressure values) or go with the default selection.STEP 2Enter the steam mass flow rate value or go with the default steam massflow rate value.STEP 3Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 4Click on the Calculate button to start the calculation of the Rankine cycleoutput values for the chosen input values.bU, (ءQSTEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1d#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+#7( Q  0 .#ءQPower Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).7 17=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 e&. ,ءQPower Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1Q19 @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 @ءQPower 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.1)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 < FءQRunning - Power Cycle Components/Processes: Compression: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.] 5 8ءQSTEP 5Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.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 : BءQPower 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.1159 @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  = HءQRunning - Power Cycle Components/Processes: Compression: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value. 7 <ءQSTEP 5Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Enter the desired compressor isentropic efficiency value or go with thedefault compressor isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1 O1O89 @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+Oc( Q J89 @ءQPower 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 compression1c1 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 5> JءQRunning - Power Cycle Components/Processes: Compression: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.STEP 5X%+ 3 4KءQEnter the desired compressor mass value or go with the defaultmass value.STEP 6Click on the Calculate button to start the calculation of compressor outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.15 1 c   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 c c . ,ءQPower Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1  1 c } 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 } ; DءQPower 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, StoichiometryOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J! ) "BءQSpecific heat is not constant.1717E,@9 @aءQEngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:7,@http://www.engineering-4e.com+7W@( Q ?,@B9 @ ءQRunning - Power Cycle Components/Processes: Combustion: Coal/OilSTEP 1Enter the desired fuel (coal or oil) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.&W@D9 @ءQFurthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired stoichiometry (1 or > 1) or go with the default stoichiometry value.STEP 6Click on the Calculate button to start the calculation of combustion gasBE- (MءQcomposition and flame temperature value for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1DE1k EHEF9 @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+EF( Q &FH< FءQPower 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, StoichiometryOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.Specific heat is not constant.1F+I1x!+IrOHJ9 @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?J( Q 2JqL9 @ءQRunning - Power Cycle Components/Processes: Combustion: GasSTEP 1Enter the desired fuel (gas) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.,?JN9 @ءQFurthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired stoichiometry value (1 or > 1) or go with the default stoichiometry value.STEP 6Click on the Calculate button to start the calculation of combustion gasqLrO. *OءQcomposition and flame temperature value for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1NO1#"ORrO9 @aءQEngineering SoftwareP.O. Box 118OrO0, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+OÀ( Q aR. ,ءQPower Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1À1#1Rl9 @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 al19 @ءQPower 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.1b1$b-1K9 @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+bv( Q K< FءQRunning - Power Cycle Components/Processes: Expansion: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine/expander inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine/expander inlet pressure value or go with thedefault pressure value.STEP 4Enter the desired turbine/expander outlet pressure value or go with thedefault pressure value.jv-5 8ءQSTEP 5Enter the desired turbine/expander mass flow rate value or go with thedefault mass flow rate value.STEP 6Click on the Calculate button to start the calculation of turbine/expanderoutlet temperature and power output values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1^1%^)-G9 @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 ~G)9 @ءQPower 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.1rZ1$&Z)C9 @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+Zn( Q C< FءQRunning - Power Cycle Components/Processes: Expansion: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine/expander inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine/expander inlet pressure value or go with thedefault pressure value.STEP 4Enter the desired turbine/expander outlet pressure value or go with thedefault pressure value. n8 >ءQSTEP 5Enter the desired turbine/expander mass flow rate value or) go with thedefault mass flow rate value.STEP 6Enter the desired turbine/expander isentropic efficiency value or go with the default turbine/expander isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of turbine/expanderoutlet temperature and power output values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back to8( ءQthe Main menu.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 |C9 @ءQPower 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 expansion1.1(@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 <+? LءQRunning - Power Cycle Components/Processes: Expansion: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired turbine mass value or go with the default@2 2ءQmass value.STEP 6Click on the Calculate button to start the calculation of turbine outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1+q1)q@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( Q yKZ. ,ءQCompressible FlowThis section provides analysis of compressible flow.1/1K*/I9 @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+/C( Q I8 >ءQCompressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1Cz1%+zIc9 @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+z( Q $c> JءQRunning - Compressible Flow: Mach NumberSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Enter the desired velocity value or go with the default velocity value.STEP 4Click on Ithe Calculate button to start the calculation of Mach numbervalue for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:) ""ءQthe Main menu.1)1,)< 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+)A( Q A 8 >ءQCompressible Flow: NozzleThis subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1A1Q-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 (> JءQRunning - Compressible Flow: NozzleSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of Mach number,/ ,kءQstagnation temperature and stagnation pressure values for the choseninput values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.11L. 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  < FءQCompressible 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 constant1 P 1/P  @ 9 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+P d ( Q K 9 ? LءQRunning - Compressible Flow: Normal ShockSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired inlet stagnation temperature value or go with thedefault inlet stagnation temperature value.STEP 3Enter the desired inlet stagnation pressure value or go with the defaultinlet stagnation pressure value.STEP 4Enter the desired inlet velocity value or go with the default velocityvalue.STEP 5Click on the Calculate button to start the calculation of inlet MachJd  @0 .5ءQnumber, inlet static temperature, inlet static pressure, outlet Machnumber, outlet velocity, outlet static temperature, and outlet staticpressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu. @ 1=@10=@B @&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+=@QA( Q E &AB8 >ءQCompressible Flow: DiffuserThis subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1QAB1C1BFBC9 @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( Q CE> JءQRunning - Compressible Flow: DiffuserSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired static temperature value or go with the default statictemperature value.STEP 3Enter the desired static pressure value or go with the default staticpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of Mach number,CF/ ,kءQstagnation temperature and stagnation pressure values for the choseninput values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1E G12 GIFG9 @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+ GH( Q zAGI9 @ءQCompressible Flow: ThrustThis 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 constant1HI13INIJ9 @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 )JM> JءQRunning - Compressible Flow: ThrustSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired mass flow rate value or go with the default mass flowpJN7 <ءQrate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1M14443Helv^ &G"F ^ 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