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Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŽE¤F( €€˜˜‚Q€ ‚˙ŮyFšH< F€ł€€‚€‚€ €‚€ €‚‚‚‚‚‚‚˙Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power and Propulsion Systems Analysis, that quickly andreliably calculates thermodynamic and transport properties of gaseous,liquid and solid species, analyzes power cycles, power cyclecomponents/processes and compressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management of٤FÍJ; D€ł€€‚‚‚‚‚‚€ €€ €‚‚€ ‚˙power and propulsion 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 PropertiesššHęLd –€s€€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚˙Temperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressurePower CyclesCarnotBrayton (Power and Propulsion)RankineOttoDieselPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowVelocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software CompatibilityeÍJyM* $€Ę€€ƒ‚ƒ‚ƒ‚ƒ‚˙80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:j:ęLăM0 0€t€‘€†üEĄ€ƒƒ‚ƒƒ‚˙Windows 98, Windows 2000, Windows ME andWindows XP ßyMîN, &€ż€€‚‚‚‚‚ƒ‚‚‚˙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.ÖĽăMÄO1 0€K€€‚€ ‚€‚‚‚‚‚‚˙Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1îN €1q˙˙˙˙˙˙˙˙˙˙˙˙ €L‡ÄO €ÄOëąÄO÷€: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€ ‚˙ Ë÷€+ƒ> J€—€†ŘĄQ€‚€‚€ €‚‚‚‚‚‚‚‚‚‚˙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:"ŕ"M…B R€Á€†ŘĄQ€‚€ €‚‚‚‚‚‚‚‚‚‚€ ‚€‚˙Thermodynamic and Transport PropertiesSingle specie 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 specie consideration -- fuel mass flow rate ignored and˙ˇ+ƒL‡H ^€o€†ŘĄQ€‚‚‚‚‚€ €‚‚‚‚‚‚€ ‚€‚‚‚€‚˙its impact on the properties of the working fluidBasic equations hold (continuity, momentum and energyequations)Specific heat is constantPower Cycle Components/ProcessesSingle specie considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constantCompressible FlowSingle specie considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constant1M…}‡1P˙˙˙˙˙˙˙˙˙˙˙˙}‡œŠëąL‡hˆ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+}‡“ˆ( €€˜˜‚Q€ ‚˙ ÎhˆœŠ; D€€†ŘĄQ€‚€‚€ ‚€‚‚‚‚‚‚˙How to Use the ProgramIn each section, subsection of the Power and Propulsion SystemsAnalysis program, the user needs to change one or more input valuesin order to calculate a new case. Input values are in boxes with whitebackground and can be changed by clicking on each individual box oreven by using the arrow keys and changing the current value. Outputvalues cannot be modified, changed by the user and they are in boxeswith black background.1“ˆÍŠ1W˙˙˙˙˙˙˙˙˙˙˙˙͊˙Ŕ뱜Џ‹: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+͊ă‹( €€˜˜‚Q€ ‚˙5󸋎B R€ç€†ŘĄQ€‚€‚€ €‚‚‚‚€ €‚‚‚‚˙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 thisAńă‹eŔP n€ă€†ŘĄQ€‚€ €€ €‚€ €€ €‚‚‚‚‚€ €‚‚˙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 EnŽeŔœŠgineering Softwareresulted from accident, abuse or misapplication of the medium, thenšmŽ˙Ŕ- *€Ú€†ŘĄQ€ €‚‚˙Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1eŔ0Á1"˙˙˙˙˙˙˙˙˙˙˙˙0Á!Ĺëą˙ŔÂ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+0ÁFÂ( €€˜˜‚Q€ ‚˙L’Â- *€>€†ŘĄQ€‚€‚˙Suggestion/Evaluation FormÜFÂŚĂ8 >€š€ †ŘĄQ€‚‚€ ‚€‚‚‚‚‚‚˙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‘]’Â7Ä4 8€ş€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:Q(ŚĂˆÄ) "€P€ †ŘĄQ€ ‚˙Power and Propulsion Systems Analysis™[7Ä!Ĺ> L€ś€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Quality:Usefulness:Possible areas of improvement:Other suggestions:1ˆÄRĹ1j˙˙˙˙˙˙˙˙˙˙˙˙RŋĘëą!Ĺ=Ć: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+RĹhĆ( €€˜˜‚Q€ ‚˙ Ü=ƈČD V€š€†ŘĄQ€‚€‚€ €‚€ €‚‚‚‚‚‚‚‚‚˙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 after youracceptance of this license. Your rights and obligations with respect tothe 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 andĎhƋĘ4 6€Ÿ€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚˙- 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 software1ˆČźĘ1ł˙˙˙˙˙˙˙˙˙˙˙˙źĘ>Î뱋ʧË: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+źĘŇË( €€˜˜‚Q€ ‚˙ß§ËçÍ6 :€ż€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚˙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.ŇË>Î) "€\€†ŘĄQ€‚˙steam table calculations are not available.1çÍoÎ1#˙˙˙˙˙˙˙˙˙˙˙˙oÎÚëą>ÎZĎ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+o΅Ď( €€˜˜‚Q€ ‚˙IZĎÚ9 @€!€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Temperature - PressureThis subsection provides ph…ĎÚ>Îysical properties of the selected specie forassigned temperature and pressure.Input Values:Specie, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1…Ď 1Ľ˙˙˙˙˙˙˙˙ ˙˙˙˙ ď˛Úú= H€e€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ€‚˙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€ ‚˙ âúE> J€Ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Temperature - PressureSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Enter the desired pressure value or go with the default pressure value.STEP 4Click on the Calculate button to start the calculation of the physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:%) "€"€†ŘĄQ€‚˙the Main menu.1E°1‡˙˙˙˙˙˙˙˙ ˙˙˙˙°ëą›: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+°Ć( €€˜˜‚Q€ ‚˙@›9 @€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Enthalpy - PressureThis subsection provides physical properties of the selected specie forassigned enthalpy and pressure.Input Values:Specie, Enthalpy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1Ć71—˙˙˙˙˙˙˙˙ ˙˙˙˙7 ëą": B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+7M( €€˜˜‚Q€ ‚˙Ů"c = H€ł€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Enthalpy - PressureSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired enthalpy value or go with the default enthalpy value.STEP 3Enter the desired pressure value or go with the default pressure value.STEP 4Click on the Calculate button to start the calculation of the physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:M ) "€"€†ŘĄQ€‚˙the Main menu.1c Î 1‚˙˙˙˙˙˙˙˙ ˙˙˙˙Î  뱝 š : B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Î ä ( €€˜˜‚Q€ ‚˙;š  8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Properties: Entropy - PressureThis subsection provides physical properties of the selected specie forassigned entropy and pressure.Input Values:Specie, Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1ä P 1Ň˙˙˙˙˙˙˙˙ ˙˙˙˙P ż@ëą ;: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+P f( €€˜˜‚Q€ ‚˙Ö;…@= H€­€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Entropy - PressureSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired entropy value or go with the default entropy value.STEP 3Enter the desired pressure value or go with the default pressure value.STEP 4Click on the Calculate button to start the calculation of the physicalpf…@ roperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:fż@) "€"€†ŘĄQ€‚˙the Main menu.1…@đ@1˙˙˙˙˙˙˙˙˙˙˙˙đ@ÎDëąż@ŰA: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+đ@B( €€˜˜‚Q€ ‚˙(íŰA.D; D€Ű€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙CoefficientsFor each reaction specie, the thermodynamic functions specific heat,enthalpy and entropy as functions of temperature are given in the form ofleast squares coefficients as follows:Cp/R = A1 + A2*T + A3*T^2 + A4*T^3 + A5*T^4 [/]H/(R*T) = A1 + A2*T/2 + A3*T^2/3 + A4*T^3/4 + A5*T^4/5 + A6/T [/]S/R = A1*lnT + A2*T + A3*T^2/2 + A4*T^3/3 + A5*T^4/4 + A7 [/]For each specie, two sets of coefficients are included for two adjecent vBÎD* $€ě€†ŘĄQ€‚‚˙temperature intervals, 273 to 1,000 K and 1,000 to 5,000 K. The data havebeen constrained to be equal at 1,000 K.1.D˙D1Ť˙˙˙˙˙˙˙˙˙˙˙˙˙DyGëąÎDęE: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+˙DF( €€˜˜‚Q€ ‚˙d,ęEyG8 >€Y€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Running: CoefficientsSTEP 1Select the desired specie or go with the default specie.STEP 2Read and/or print the coefficients for the calculation of the physicalproperties for the chosen specie.STEP 3When done with Steps 1 through 2, click on the Exit button to go back tothe Main menu.1FŞG1˙˙˙˙˙˙˙˙˙˙˙˙ŞGˆIëąyG•H: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ŞGŔH( €€˜˜‚Q€ ‚˙Ș•HˆI0 .€1€†ŘĄQ€‚€‚‚‚˙Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1ŔHšI1˙˙˙˙˙˙˙˙˙˙˙˙šIŠL빈I¤J: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+šIĎJ( €€˜˜‚Q€ ‚˙ťƒ¤JŠL8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙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 Properties1ĎJťL1Š˙˙˙˙˙˙˙˙˙˙˙˙ťL €뱊LŚM: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ťLŃM( €€˜˜‚Q€ ‚˙ ĚŚMÚO= H€™€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Steam Approximations:Saturated Area: Temperature DependentSTEP 1Enter the desired saturated steam temperature value or go with the defaulttemperature value.STEP 2Enter the desired steam quality or go with the default steam quality value.STEP 3Click on the Calculate button to start the calculation of the steam propertiesfor the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back to:ŃM €) "€"€†ŘĄQ€ÚO €ŠL‚˙the Main menu.1ÚOQ€1W˙˙˙˙˙˙˙˙˙˙˙˙Q€wƒëą €<: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€g( €€˜˜‚Q€ ‚˙Ň<wƒ> J€Ľ€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Steam Approximations:Saturated Area: Pressure DependentSTEP 1Enter the desired saturated steam pressure value or go with the defaultpressure value.STEP 2Enter the desired steam quality or go with the default steam quality value.STEP 3Click on the Calculate button to start the calculation of the steamproperties for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1g¨ƒ1Š˙˙˙˙˙˙˙˙˙˙˙˙¨ƒ †ëąwƒ“„: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+¨ƒž„( €€˜˜‚Q€ ‚˙b,“„ †6 :€Y€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚˙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 Properties1ž„Q†1Y˙˙˙˙˙˙˙˙˙˙˙˙Q†y‰ëą †<‡: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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†g‡( €€˜˜‚Q€ ‚˙Ő<‡y‰= H€Ť€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Steam Approximations: Superheated AreaSTEP 1Enter the desired superheated steam temperature value or go with the defaulttemperature value.STEP 2Enter the desired superheated steam pressure value or go with the defaultpressure value.STEP 3Click on the Calculate button to start the calculation of the steamproperties for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1g‡މ1é˙˙˙˙˙˙˙˙˙˙˙˙މb‹ëąy‰•Š: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+މŔŠ( €€˜˜‚Q€ ‚˙˘s•Šb‹/ .€ć€†ŘĄQ€‚€‚‚‚˙Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto and Diesel).1ŔŠ“‹1Î˙˙˙˙˙˙˙˙˙˙˙˙“‹0Žëąb‹~Œ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+“‹Ќ( €€˜˜‚Q€ ‚˙‡N~Œ0Ž9 @€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙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.1ЌaŽ1 ˙˙˙˙˙˙˙˙˙˙˙˙aŽŒÁëą0ŽL: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+aŽw( €€˜˜‚Q€ ‚˙ ĚLŒÁ= H€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: CarnotSTEP 1Enter the desired heat addition wŒÁ0Žtemperature 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.1w˝Á1˙˙˙˙˙˙˙˙˙˙˙˙˝ÁŒĂ뱌Á¨Â: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+˝ÁÓÂ( €€˜˜‚Q€ ‚˙š‰¨ÂŒĂ0 .€€†ŘĄQ€‚€‚‚‚˙Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1Ó½Ă1˙˙˙˙˙˙˙˙˙˙˙˙˝Ă’Ç뱌èÄ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+˝ĂÓÄ( €€˜˜‚Q€ ‚˙ۨÄéĆ; D€ˇ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.ŠÓÄ’Ç* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1éĆĂÇ1k˙˙˙˙˙˙˙˙˙˙˙˙ĂÇýĚ뱒ÇŽČ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ĂÇŮČ( €€˜˜‚Q€ ‚˙@ŽČË? L€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - 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 defaultäŤŮČýĚ9 @€W€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙turbine 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.1Ë.Í1.˙˙˙˙˙˙˙˙˙˙˙˙.ÍëąýĚÎ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+.ÍDÎ( €€˜˜‚Q€ ‚˙ÚÎe; D€ľ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RatDÎeýĚeAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.ŠDÎ* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1e?1j˙˙˙˙˙˙˙˙˙˙˙˙?xëą*: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€ ‚˙?*”? L€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Power (Real)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 defaultäŤUx9 @€W€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙turbine 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”Š1˙˙˙˙˙˙˙˙˙˙˙˙Š“ ëąx”: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Šż( €€˜˜‚Q€ ‚˙9ý”ř < F€ű€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 power›qż“ * $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ř Ä 1p˙˙˙˙˙˙˙˙˙˙˙˙Ä @뱓 Ż : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Ä Ú ( €€˜˜‚Q€ ‚˙EŻ ? L€ €†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Propulsion (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 defaultäŤÚ @9 @€W€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙turbine 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˙˙˙˙˙˙˙˙ ˙˙˙˙@@)Dëą@+A: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+@@VA( €€˜˜‚Q€ ‚˙8ü+AŽC< F€ů€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 HHVOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine power›qVA)D* $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ŽCZD1o˙˙˙˙˙˙˙˙!˙˙˙˙ZD˜Iëą)DEE: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ZDpE( €€˜˜‚Q€ ‚˙DEE´G? L€ €†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Propulsion (Real)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 defaultäŤpE˜I9 @€W€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙turbine 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´GÉI1Ü˙˙˙˙˙˙˙˙"˙˙˙˙ÉItL빘I´J: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ÉIßJ( €€˜˜‚Q€ ‚˙•[´JtL: B€ˇ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.1ßJĽL1 ˙˙˙˙˙˙˙˙#˙˙˙˙ĽLd€ëątLM: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ĽLťM( €€˜˜‚Q€ ‚˙ӐMĘO< F€§€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - 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.ŽbťMd€, (€Ä€†ŘĄQ€‚‚‚‚˙STEP 5WĘOd€tLhen done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1ĘO•€1Ű˙˙˙˙˙˙˙˙$˙˙˙˙•€?„ëąd€€: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+•€Ť( €€˜˜‚Q€‚˙*ń€Ճ9 @€ă€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: OttoThis subsection provides analysis of the Otto cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Revolutions, Fuel HHVNumber 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?Ť?„+ &€~€†ŘĄQ€‚‚‚˙Assumptions:Specific heat is constant. Four stroke engine.1Ճp„1ˇ˙˙˙˙˙˙˙˙%˙˙˙˙p„öŠëą?„[…: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+p„†…( €€˜˜‚Q€ ‚˙)ę[…݇? L€Ő€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: OttoSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired combustion temperature value or go with the default!内Љ< F€Ë€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙temperature value.STEP 6Enter the desired number of revolutions value or go with the defaultnumber of revolutions value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the desired number of cylinders value or go with the default numberof cylinders value.STEP 9Enter the desired cylinder stroke value or go with the default cylinderstroke value.STEP 10Enter the desired stroke to diameter value or go with the default stroke&ô݇öŠ2 2€é€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙to diameter value.STEP 11Click on the Calculate button to start the calculation of the Otto 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.1Љ'‹1ń˙˙˙˙˙˙˙˙&˙˙˙˙'‹çŽëąöŠŒ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+'‹=Œ( €€˜˜‚Q€ ‚˙2ůŒoŽ9 @€ó€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: DieselThis 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, FuelxL=ŒçŽ, (€˜€†ŘĄQ€‚‚‚‚˙ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1oŽ1Í˙˙˙˙˙˙˙˙'˙˙˙˙ŔĹëąçŽŔ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.coŔçŽm+:Ŕ( €€˜˜‚Q€ ‚˙/đŔiÂ? L€á€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: DieselSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired cut-off ratio (volumetric) value or go with the default,đ:Ŕ•Ä< F€á€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙cut-off ratio value.STEP 6Enter the desired number of revolutions value or go with the defaultnumber of revolutions value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the desired number of cylinders value or go with the default numberof cylinders value.STEP 9Enter the desired cylinder stroke value or go with the default cylinderstroke value.STEP 10Enter the desired stroke to diameter ratio value or go with the default stroke to+ůiÂŔĹ2 2€ó€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙diameter ratio value.STEP 11Click on the Calculate button to start the calculation of the Diesel 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.1•ÄńĹ1•˙˙˙˙˙˙˙˙(˙˙˙˙ńĹUĘëąŔĹÜĆ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ńĹÇ( €€˜˜‚Q€ ‚˙2ůÜĆ9É9 @€ó€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙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 Length, MobilityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Hall Voltage, Outlet StaticTemperature, Outlet Static Pressure, Outlet Mach Number, OutletíÇUĘ/ ,€Ű€†ŘĄQ€‚‚‚‚‚‚˙Stagnation Temperature, Outlet Stagnation Pressure, Specific WorkOutput, Enthalpy ExtractionAssumptions:Specific heat, velocity, conductivity, mobility, induced voltage field, Hallvoltage and magnetic field strength are constant.19ɆĘ1_˙˙˙˙˙˙˙˙)˙˙˙˙†Ę´ëąUĘqË: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+†ĘœË( €€˜˜‚Q€ ‚˙4öqËĐÍ> J€í€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: MagnetohydrodynamicsSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired inlet stagnation temperature value or go with the defaulttemperature value.STEP 3Enter the desired inlet stagnation pressure value or go with the defaultpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired conductivity value or go with the default conductivity value.H œË$< F€€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 6Enter the desired loading parameter value or go with the default loadingparameter value.STEP 7Enter the desired magnetic field strength value or go with the defaultmagnetic field strength value.STEP 8Enter the desired channel length value or go with the default channellength value.STEP 9Enter the desired mobility value or go with the default mobility value.STEP 10Click on the Calculate button to start the calculation of the Magnetohydrodynamics cycle output values for thĐÍ$UĘe chosen input values.dĐÍ´, (€Č€†ŘĄQ€‚‚‚‚˙STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1$ĺ1Â˙˙˙˙˙˙˙˙*˙˙˙˙ĺvëą´Đ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ĺű( €€˜˜‚Q€ ‚˙ßĐ / ,€ż€€‚€‚‚‚‚‚‚‚‚˙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:mDűv) "€ˆ€†ŘĄQ€‚˙Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1 §1˙˙˙˙˙˙˙˙+˙˙˙˙§ëąv’: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€ ‚˙ á’Ý? L€Ă€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Fuel CellSTEP 1Select the desired fuel (working fluid) or go with the default selection.STEP 2Enter the desired fuel inlet temperature or go with the defaulttemperature value.STEP 3Enter the desired oxidant inlet temperature value or go with the defaulttemperature value.STEP 4Enter the desired fuel flow rate or go with the default fuel flow ratevalue.STEP 5Enter the desired product outlet temperature value or go with the default(ö˝2 2€í€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙temperature value.STEP 6Click on the Calculate button to start the calculation of the Fuel Cell cycleoutput 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.1Ý61˙˙˙˙˙˙˙˙,˙˙˙˙6 ëą! : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+6L ( €€˜˜‚Q€ ‚˙Á‘!  0 .€#€†ŘĄQ€‚€‚‚‚˙Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1L > 1Ú˙˙˙˙˙˙˙˙-˙˙˙˙> ç ëą ) : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+> T ( €€˜˜‚Q€ ‚˙“e) ç . ,€Ę€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1T  1ô˙˙˙˙˙˙˙˙.˙˙˙˙ Űëąç  : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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 Ű= H€á€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processes:Compression: Isentropic (Ideal)This subsection provides analysis of isentropic compression.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1.  1Ř˙˙˙˙˙˙˙˙/˙˙˙˙ ČCëąŰ @: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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  @Ű+ 7@( €€˜˜‚Q€ ‚˙ Ç @@BB R€€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Compression: Isentropic (Ideal)STEP 1Select the desired specie 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 compressor outlet pressure value or go with the defaultpressure value.STEP 5ˆU7@ČC3 4€Ť€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚˙Enter 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.1@BůC1ó˙˙˙˙˙˙˙˙0˙˙˙˙ůCťFëąČCäD: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ůCE( €€˜˜‚Q€ ‚˙ŹoäDťF= H€ß€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processes:Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1EěF1×˙˙˙˙˙˙˙˙1˙˙˙˙ěF’KëąťF×G: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ěFH( €€˜˜‚Q€ ‚˙Ć×G JB R€€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Compression: Isentropic (Real)STEP 1Select the desired specie 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 compressor outlet pressure value or go with the defaultpressure value.STEP 5ˆUH’K3 4€Ť€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚˙Enter 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.1 JĂK1×˙˙˙˙˙˙˙˙2˙˙˙˙ĂKiN뱒KŽL: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ĂKŮL( €€˜˜‚Q€ ‚˙SŽLiN= H€§€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processs:Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid (Specie), Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression1ŮLšN1X˙˙˙˙˙˙˙˙3˙˙˙˙šNƒëąiN…O: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+šN°O( €€˜˜‚Q€ ‚˙Aţ…OýC T€ý€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - °OýiNPower CycleComponents/Processes:Compression: IsothermalSTEP 1Select the desired specie 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 compressor outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired compressor mass value or go with the defaultć°Oƒ2 2€Í€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙mass 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.1ýFƒ1Ř˙˙˙˙˙˙˙˙4˙˙˙˙Fƒí„ëąƒ1„: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Fƒ\„( €€˜˜‚Q€ ‚˙‘c1„í„. ,€Ć€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1\„…1Š˙˙˙˙˙˙˙˙5˙˙˙˙…–ˆëąí„ †: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+…4†( €€˜˜‚Q€ ‚˙Ů †Lˆ? L€ł€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/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, Oxidant to Fuel RatioOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Stoichiometry, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!4†–ˆ) "€B€†ŘĄQ€‚˙Specific heat is not constant.1LˆLj1˙˙˙˙˙˙˙˙6˙˙˙˙Lj뱖ˆ˛‰: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Lj݉( €€˜˜‚Q€ ‚˙B˛‰Œ< F€ €†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/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.%ë݉DŽ: B€×€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Furthermore, click on the fuel Normalize button one more time tocalculate the new stoichiometry 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 oxidant to fuel ratio ( > 1) or go with the default oxidantto fuel ratio.STEP 6Click on the Calculate button to start the calculation of combustion gasÓŚŒ- (€M€†ŘĄQ€‚‚‚‚˙composition 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.1DŽH1œ˙˙˙˙˙˙˙˙7˙˙˙˙HżÂ뱏?Ŕ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineeriH?Ŕng-4e.comWeb Site:http://www.engineering-4e.com+HjŔ( €€˜˜‚Q€ ‚˙ Ě?ŔuÂ? L€™€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/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, Oxidant to Fuel RatioOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Stoichiometry, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!jŔżÂ) "€B€†ŘĄQ€‚˙Specific heat is not constant.1uÂđÂ1x˙˙˙˙˙˙˙˙8˙˙˙˙đÂ7ÉëążÂŰĂ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+đÂÄ( €€˜˜‚Q€ ‚˙7úŰĂ=Ć= H€ő€†ŘĄQ€‚ƒ‚ƒ€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/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.%ëÄbČ: B€×€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Furthermore, click on the fuel Normalize button one more time tocalculate the new stoichiometry 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 oxidant to fuel ratio ( > 1) or go with the default oxidantto fuel ratio.STEP 6Click on the Calculate button to start the calculation of combustion gasŐ§=Ć7É. *€O€†ŘĄQ€‚‚‚‚‚˙composition 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.1bČhÉ1Ö˙˙˙˙˙˙˙˙9˙˙˙˙hÉ Ëëą7ÉSĘ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+hÉ~Ę( €€˜˜‚Q€ ‚˙aSĘ Ë. ,€Â€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1~Ę>Ë1ď˙˙˙˙˙˙˙˙:˙˙˙˙>ËüÍëą Ë)Ě: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+>ËTĚ( €€˜˜‚Q€ ‚˙¨k)ĚüÍ= H€×€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processes:Expansion: Isentropic (Ideal)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1TĚ-Î1.˙˙˙˙˙˙˙˙;˙˙˙˙-Î ëąüÍĎ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+-ÎCĎ( €€˜˜‚Q€ ‚˙ßĎn@ N€ż€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Expansion: Isentropic (Ideal)STEP 1Select the desired specie (working fCĎnüÍluid) or go with the default specie.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.ŸjCĎ 5 8€Ő€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 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.1n>1î˙˙˙˙˙˙˙˙<˙˙˙˙>űëą ): B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+>T( €€˜˜‚Q€ ‚˙§j)ű= H€Ő€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processes:Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1T,1˙˙˙˙˙˙˙˙=˙˙˙˙,˙ ëąű: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+,B( €€˜˜‚Q€ ‚˙Ţ` @ N€˝€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Expansion: Isentropic (Real)STEP 1Select the desired specie (working fluid) or go with the default specie.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.ŸjB˙ 5 8€Ő€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 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` 0 1“˙˙˙˙˙˙˙˙>˙˙˙˙0 ’ ëą˙  : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+0 F ( €€˜˜‚Q€ ‚˙L ’ ; D€#€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processs:Expansion: IsothermalInput Values:Working Fluid (Specie), Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal expansion1F Ă 1k˙˙˙˙˙˙˙˙?˙˙˙˙Ă -B뱒 Ž: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Ă Ů( €€˜˜‚Q€ ‚˙3đŽAC T€á€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Expansion: IsothermalSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired turbine inlet temperature value or go with thedefault temperatuŮA’ re 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 defaultăŮ-B2 2€Ç€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙mass 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.1A^B1M˙˙˙˙˙˙˙˙@˙˙˙˙^BzEëą-BIC: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+^BtC( €€˜˜‚Q€ ‚˙ËICzE; D€—€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Heat TransferThis subsection provides analysis of heat transfer.Input Values:Hot Working Fluid (Specie), Hot Working Fluid Mass Flow Rate, HotWorking Fluid Inlet Temperature, Hot Working Fluid Outlet Temperature,Cold Working Fluid (Specie), Cold Working Fluid Mass Flow Rate, ColdWorking Fluid Inlet TemperatureOutput Values:Cold Working Fluid Outlet TemperatureAssumptions:Ideal heat transfer -- no losses1tCŤE1Ü˙˙˙˙˙˙˙˙A˙˙˙˙ŤEVKëązE–F: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ŤEÁF( €€˜˜‚Q€ ‚˙ß–FßH? L€ż€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes: Heat TransferSTEP 1Select the desired hot specie (hot working fluid) or go with the defaultspecie.STEP 2Enter the desired hot working fluid mass flow rate or go with the defaultmass flow rate value.STEP 3Enter the desired hot working fluid inlet temperature value or go with thedefault temperature value.STEP 4Enter the desired hot working fluid outlet temperature value or go with thedefault temperature value.=ÁFK< F€€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 5Select the desired cold specie (cold working fluid) or go with the defaultspecie.STEP 6Enter the desired cold working fluid mass flow rate or go with the defaultmass flow rate value.STEP 7Enter the desired cold working fluid inlet temperature value or go with thedefault temperature value.STEP 8Click on the Calculate button to start the calculation of heat transfer outletvalues for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back to:ßHVK) "€"€†ŘĄQ€‚˙the Main menu.1K‡K1 ˙˙˙˙˙˙˙˙B˙˙˙˙‡K`NëąVKrL: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+‡KL( €€˜˜‚Q€ ‚˙ÉrL`N: B€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: MixingThis subsection provides analysis of mixing.Input Values:Inlet Working Fluids (Species), Inlet Working Fluids Mass Flow Rate, InletWorking Fluids Temperature, Outlet Working Fluids (Species), Outlet WorkingFluids Mass Flow RateOutput Values:Outlet Working Fluids Temperature -- Mixing TemperatureAssumptions:Ideal mixing -- no losses1L‘N1â˙˙˙˙˙˙˙˙C˙˙˙˙‘NŃëą`N|O: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+‘N§O( €€˜˜‚Q€ ‚˙Ô|OŁ> J€Š€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleC§OŁ`Nomponents/Processes: MixingSTEP 1Select the desired inlet species (inlet working fluids) or go with the defaultspecies.STEP 2Enter the desired inlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 3Enter the desired inlet working fluids inlet temperature values or go with thedefault temperature values.STEP 4Enter the desired hot working fluid outlet temperature value or go with theƧOŃ: B€€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙default temperature value.STEP 5Select the desired outlet species (outlet working fluid) or go with the defaultspecies.STEP 6Enter the desired outlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 7Click on the Calculate button to start the calculation of mixing outletvalues for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1Łöƒ1Ŕ˙˙˙˙˙˙˙˙D˙˙˙˙öƒ……ëąĹƒá„: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+öƒ …( €€˜˜‚Q€ ‚˙yKá„……. ,€–€†ŘĄQ€‚€‚‚˙Compressible FlowThis section provides analysis of compressible flow.1 …ś…1R˙˙˙˙˙˙˙˙E˙˙˙˙ś…ׇ뱅…Ą†: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ś…̆( €€˜˜‚Q€ ‚˙ ÓĄ†ׇ8 >€§€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Velocity of SoundThis section provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1̆ˆ15˙˙˙˙˙˙˙˙F˙˙˙˙ˆ ‹ëą×‡óˆ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ˆ‰( €€˜˜‚Q€ ‚˙î˛óˆ ‹< F€e€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Velocity of SoundSTEP 1Select the desired working fluid (specie) or go with the default value.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Click on the Calculate button to start the calculation of velocity of soundvalue for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1‰=‹1M˙˙˙˙˙˙˙˙G˙˙˙˙=‹Yëą ‹(Œ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+=‹SŒ( €€˜˜‚Q€ ‚˙Î(ŒY8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1SŒŠ1;˙˙˙˙˙˙˙˙H˙˙˙˙Š ÁëąYuŽ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Š Ž( €€˜˜‚Q€ ‚˙%çuŽŃŔ> J€Ď€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Mach NumberSTEP 1Select the desired working fluid (specie) or go with the default value.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 ŽŃŔY.STEP 4Click on the 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: Ž Á) "€"€†ŘĄQ€‚˙the Main menu.1ŃŔ<Á1˙˙˙˙˙˙˙˙I˙˙˙˙<Á Ăëą Á'Â: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+<ÁRÂ( €€˜˜‚Q€ ‚˙ť‹' Ă0 .€€†ŘĄQ€‚€‚‚‚˙Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1RÂ>Ă1Š˙˙˙˙˙˙˙˙J˙˙˙˙>Ă—Ĺëą Ă)Ä: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+>ĂTÄ( €€˜˜‚Q€ ‚˙C )Ä—Ĺ8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙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 constant1TÄČĹ1I˙˙˙˙˙˙˙˙K˙˙˙˙ČĹŕÉ뱗ĹłĆ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ČĹŢĆ( €€˜˜‚Q€ ‚˙*ęłĆÉ@ N€Ő€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow:Properties: StagnationSTEP 1Select the desired working fluid (specie) or go with the default value.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 stagnationŘŞŢĆŕÉ. *€U€†ŘĄQ€‚‚‚‚‚˙temperature and stagnation pressure 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.1ÉĘ1~˙˙˙˙˙˙˙˙L˙˙˙˙Ę^ĚëąŕÉüĘ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+Ę'Ë( €€˜˜‚Q€ ‚˙7˙üĘ^Ě8 >€˙€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙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'ˏĚ1Ä˙˙˙˙˙˙˙˙M˙˙˙˙Ěľëą^ĚzÍ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ĚĽÍ( €€˜˜‚Q€ ‚˙0ňzÍŐĎ> J€ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Properties: StaticSTEP 1Select the desired working fluid (specie) or go with the default value.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 staticÔŚĽÍľ. *€M€†ŘĄQ€‚‚‚ŐĎľ^Ě‚‚˙temperature and static pressure 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.1ŐĎć1ˆ˙˙˙˙˙˙˙˙N˙˙˙˙ć=ëąľŃ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ćü( €€˜˜‚Q€ ‚˙A Ń=8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible 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 constant1ün1T˙˙˙˙˙˙˙˙O˙˙˙˙n‘ëą=Y: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+n„( €€˜˜‚Q€ ‚˙)ëY­> J€×€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: NozzleSTEP 1Select the desired working fluid (specie) or go with the default value.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,䵄‘/ ,€k€†ŘĄQ€‚‚‚‚‚‚˙stagnation 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.1­Â1M˙˙˙˙˙˙˙˙P˙˙˙˙ÂŢ 뱑­: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ÂŘ( €€˜˜‚Q€ ‚˙Ę­Ţ < F€•€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 StaticPressure, Inlet Mach NumberOutlet Stagnation Temperature, Outlet Stagnation Pressure, OutletVelocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1Ř 1á˙˙˙˙˙˙˙˙Q˙˙˙˙ żëąŢ ú : B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€ ‚˙ Ěú /> J€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Normal ShockSTEP 1Select the desired working fluid (specie) or go with the default selection.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 5_% ż1 0€ż€†ŘĄQ€‚‚‚‚‚‚‚‚˙Click on the Calculate button to start the calculation of inlet Machnumber, 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/ @17˙˙˙˙˙˙˙˙R˙˙˙˙ @gBż @żëąż÷@: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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€ ‚˙E ÷@gB8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible 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 constant1"A˜B1F˙˙˙˙˙˙˙˙S˙˙˙˙˜B­FëągBƒC: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+˜BŽC( €€˜˜‚Q€ ‚˙݃CÉE> J€ť€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: DiffuserSTEP 1Select the desired working fluid (specie) or go with the default value.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,侎C­F/ ,€k€†ŘĄQ€‚‚‚‚‚‚˙stagnation 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.1ÉEŢF1Á˙˙˙˙˙˙˙˙T˙˙˙˙ŢFnIëą­FÉG: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ŢFôG( €€˜˜‚Q€ ‚˙zAÉGnI9 @€ƒ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible 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 constant1ôGŸI1˙˙˙˙˙˙˙˙U˙˙˙˙ŸIŠNëąnIŠJ: B€c€†ŘĄQ€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙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+ŸIľJ( €€˜˜‚Q€ ‚˙.đŠJăL> J€á€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: ThrustSTEP 1Select the desired working fluid (specie) or go with the default selection.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 flow§pľJŠN7 <€á€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙rate 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 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