?_t˙˙˙˙Đłd[l‹ ÎM!Energy Conversion ... - TutorialEngineering Software (c) 1996/&;)z460&ǘ^‹F ˙˙Ż˙˙˙˙|CONTEXTĄŤ|CTXOMAPgŁ|FONTNn|SYSTEM|TOPICŁ|TTLBTREErŁšO[+˙˙ŽÇBŇ˙˙˙˙â†ÇB ˙D€†ŘĄQage D bNews-#c T[+%P[+˙˙ ‹ÇBE˙˙˙˙̈ÇBNi_nowidctlparcs16super#Engineering Softwareo%˙˙˙˙˙˙˙˙4˙˙˙˙˙˙˙˙˙˙˙˙-# Œ[+-#ЍÇB5[+=Q[+˙˙΋ÇBF˙˙˙˙Ö‹ÇB-#DÇBI-#[+˙˙¨[+°D[+˙˙dŽÇB˜˙˙˙˙DˆÇBN [+˙˙€†ŘĄQ˙˙΋ÇB  ÇB€†ŘĄQ˜‡ÇBgs V€†ŘĄQgs Bold-#LogoË [+ÓJ[+˙˙ȌÇBÓ˙˙˙˙BˆÇBd%C Le˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙˙sko eig-#MoosÎ [+ÖK[+˙˙öŒÇB-#˙˙îÜ[+äG[+˙˙ÇB(˙˙˙˙>†ÇB ˙˙€†ŘĄQCAC ç [+ďK[+˙˙z’ÇBÔ˙˙˙˙öŒÇBru VCA€†ŘĄQ&_GoudyOlSt BT'_PosterBodoni BT(_PosterBodoni It BT)bFutura Md BT*-#ra Xě[+ôP[+˙˙ÇB"˙˙˙˙‹ÇB u€ †ŘĄQ-#FutuÜ[+äO[+˙˙ ÇBÓ˙˙˙˙ŹŠÇB nowidctlparcs16˙super#-#Ťi˘i˙˙˙˙ 1˙˙˙˙=1*˙˙˙˙˙˙˙˙=nIé° &9 @€a€†ŘĄQ€€‚€‚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.comH#=n% €F€°°€‚˙Energy Conversion 1.1 - TutorialHş&śŽ ę€u€˜˜ă\ŞÓP€‰€‚ăS?€‰€‚ă$çdI€‰€‚ăĚ˙§n€‰€‚ă\–€‰€‚ăf˘v´€‰€‚〉€‚€ƒă> € ‰€ ‚˙Program DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPropertiesTemperature - Pressure\+n1 2€V€€ƒƒăŒ€ ‰€ ‚˙Running - Temperature - PressureMś_2 4€6€°˜€ƒă? € ‰€ ‚˙Enthalpy - PressureY(¸1 2€P€€ ƒƒăˇ€ ‰€ ‚˙Running - Enthalpy - PressureL_2 4€4€°˜€ƒă@ € ‰€ ‚˙Entropy - PressureX'¸\1 2€N€€ƒƒă⍀ ‰€ ‚˙Running - Entropy - PressureF˘2 4€(€°˜€ƒăA € ‰€ ‚˙CoefficientsR!\ô1 2€B€€ƒƒă Ž€ ‰€ ‚˙Running - Coefficientsn/˘b? N€^€˜˜ă€‰€‚€ƒăw€ ‰€ ‚˙Steam ApproximationsSaturated Areaąqô@ P€â€€ƒƒăNĺů€ ‰€ ‚€ ƒƒăyĺů‰€ ‚˙Running - Saturated Area - Temperature DependentRunning - Saturated Area - Pressure DependentJb]2 4€0€°˜€ƒăx€ ‰€ ‚˙Superheated AreaV%ł1 2€J€€ƒƒăJÄ€ ‰€ ‚˙Running - Superheated Area^]? N€>€˜˜ă€‰€‚€ƒă°€ ‰€ ‚˙Power CyclesCarnotR!łc1 2€B€€ƒƒă˛ú€ ‰€ ‚˙Running - Carnot CycleA¤2 4€€°˜€ƒăą€ ‰€ ‚˙BraytonIcí3 6€,€˜˜€ƒƒănŤ€ ‰€ ‚˙Power (Ideal)e3¤R2 4€f€€ƒƒƒăœGž€ ‰€ ‚˙Running - Brayton Cycle: Power (Ideal)Híš3 6€*€°˜€ƒƒăoŤ€ ‰€ ‚˙Power (Real)d2Rţ2 4€d€€ ƒƒƒăÇGž€ ‰€ ‚˙Running - Brayton Cycle: Power (Real)JšH 0 0€4€°˜€ ƒƒăpŤ‰€ ‚˙Propulsion (Ideal)j8ţ˛ 2 4€p€€ ƒƒƒăňGž€ ‰€ ‚˙Running - Brayton Cycle: Propulsion (Ideal)IH ű 0 0€2€°˜€ ƒƒăqŤ‰€ ‚˙Propulsion (Real)i7˛ d 2 4€n€€ ƒƒƒăHž€ ‰€ ‚˙Running - Brayton Cycle: Propulsion (Real)=ű Ą / .€€°˜€ ƒă˛‰€ ‚˙RankineS"d ô 1 2€D€€ ƒƒăű€ ‰€ ‚˙Running - Rankine Cycle: Ą . / .€€°˜€ ƒăł‰€ ‚˙OttoPô ~ 1 2€>€€ ƒƒă3ű€ ‰€ ‚˙Running - Otto Cycle< . ş / .€€°˜€ ƒă´‰€ ‚˙DieselR!~ 1 2€B€€ ƒƒă^ű€ ‰€ ‚˙Running - Diesel CycleJş V / .€6€°˜€ ƒăľ‰€ ‚˙Magnetohydrodynamics`/ ś 1 2€^€€ ƒƒă‰ű€ ‰€ ‚˙Running - Magnetohydrodynamics Cycle?V ő / .€ €°˜€ ƒăś‰€ ‚˙Fuel CellU$ś J 1 2€H€€ ƒƒă´ű€ ‰€ ‚˙Running - Fuel Cell CycleŸQő é N l€˘€˜˜ă€‰€‚€ƒăé€ ‰€ ‚€ ƒƒăćB߉€ ‚˙Power Cycle Components/ProcessesCompressionIsentropic (Ideal)h6J Q2 4€l€€ ƒƒƒăÄ<€%€ ‰€ ‚˙Running - Compression: Isentropic (Ideal)Ié š0 0€2€°˜€ ƒƒăçB߉€ ‚˙Isentropic (Real)g5Q2 4€j€€ ƒƒƒăď<€%€ ‰€ ‚˙Running - Compression: Isentropic (Real)BšC0 0€$€°˜€ ƒƒăčB߉€ ‚˙Isothermal`.Ł2 4€\€€ ƒƒƒă=€%€ ‰€ ‚˙Running - Compression: Isothermal@C @/ .€"€°˜€ ƒăꉀ ‚˙CombustionŁ @ @ŁL@0 0€ €˜˜€ ƒƒăJ߉€ ‚˙Coal/Oil]+ @Š@2 4€V€€ ƒƒƒăWs%€ ‰€ ‚˙Running - Combustion: Coal/Oil; L@ä@0 0€€°˜€ ƒƒă J߉€ ‚˙GasX&Š@lFG0 0€€°˜€ ƒƒă |‰€ ‚˙StaticY'ÉF`G2 4€N€€ ƒƒƒăĐŐE.€ ‰€ ‚˙Running - Static Properties< GœG/ .€€°˜€ ƒă%&‰€ ‚˙NozzleL`GčG1 2€6€€ ƒƒăYh€ ‰€ ‚˙Running - NozzleBœG*H/ .€&€°˜€ ƒă&&‰€ ‚˙Normal ShockR!čG|H1 2€B€€ ƒƒă„h€ ‰€ ‚˙Running - Normal Shock>*HşH/ .€€°˜€ ƒă'&‰€ ‚˙DiffuserN|HI1 2€:€€ ƒƒăŻh€ ‰€ ‚˙Running - Diffuser< şHDI/ .€€°˜€ ƒă(&‰€ ‚˙ThrustLII1 2€6€€ ƒƒăÚh€ ‰€ ‚˙Running - Thrust1DIÁI1> ˙˙˙˙˙˙˙˙˙˙˙˙ÁIڅ鰐IŞJ9 @€a€†ŘĄQ€€‚€‚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+ÁIŐJ( €€˜˜‚Q€ ‚˙7üŞJ M; D€ů€€‚€‚€ €‚€ €‚‚‚‚‚‚˙Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Energy Conversion, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, contains coefficients for the calculation of the physicalproperties of various species -- the user has the capability to use thecoefficients to carry out independent engineering calculations involvingphysical properties of various species, steam approximations, analyzesěŐJ#O+ $€Ů€€‚‚‚‚‚‚‚‚˙power cycles, power cycle components/processes and compressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunityto more quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outŔ MHY €€€€‚€ €€ €‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚˙more about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (3#OHI01) 540-3605.Thermodynamic and Transport PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressureCoefficientsSteam ApproximationsSaturated Area (Temperature and Pressure Dependent)Superheated AreaPower CyclesCarnotBrayton (Power and Propulsion) §#ORƒc ”€O€€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚˙RankineOttoDieselMagnetohydrodynamicsFuel CellPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionHeat TransferMixingCompressible FlowVelocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard drive?H‘ƒ$ €6€€ƒ‚˙IBM compatible systems:h:Rƒůƒ. ,€t€†üEĄ€ƒƒ‚ƒƒ‚˙Windows 98, Windows 2000, Windows ME andWindows XP ߑƒ…, &€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.ÖĽůƒÚ…1 0€K€€‚€ ‚€‚‚‚‚‚‚˙Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1… †1o˙˙˙˙˙˙˙˙˙˙˙˙ †Ié°Ú…ô†9 @€a€†ŘĄQ€€‚€‚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€ ‚˙ Ëô†(‰> 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‡J‹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(‰I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 constant1J‹z19˙˙˙˙˙˙˙˙˙˙˙˙zŽŔé°IcŽ9 @€a€†ŘĄQ€€‚€‚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+zŽŽ( €€˜˜‚Q€ ‚˙ôşcŽŽŔ: B€u€†ŘĄQ€‚€‚€ €‚‚‚‚‚‚˙How to Use the ProgramIn each section, subsection of the Energy Conversion program, theuser needs to change one or more input values in order to calculate anew case. Input values are in boxes with white background and can bechanged by clicking on each individual box or even by using the arrowkeys andŽŽŽŔI changing the current value. Output values cannot be modified,changed by the user and they are in boxes with black background.1ŽŽżŔ1U˙˙˙˙˙˙˙˙˙˙˙˙żŔăĆ鰎Ŕ¨Á9 @€a€†ŘĄQ€€‚€‚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+żŔÓÁ( €€˜˜‚Q€ ‚˙5ó¨ÁÄB 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 thisAńÓÁIĆP 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 Engineering Softwareresulted from accident, abuse or misapplication of the medium, thenšmÄăĆ- *€Ú€†ŘĄQ€ €‚‚˙Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1IĆÇ1 ˙˙˙˙˙˙˙˙˙˙˙˙ÇíĘé°ăĆýÇ9 @€a€†ŘĄQ€€‚€‚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+Ç(Č( €€˜˜‚Q€ ‚˙LýÇtČ- *€>€†ŘĄQ€‚€‚˙Suggestion/Evaluation FormÜ(ȈÉ8 >€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‘]tČĘ4 8€ş€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:=ˆÉVĘ) "€(€ †ŘĄQ€ ‚˙Energy Conversion—ZĘíĘ= J€´€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Quality:Usefulness:Possible areas of improvement:Other suggestions:1VĘË1p˙˙˙˙˙˙˙˙˙˙˙˙Ëaé°íĘĚ9 @€a€†ŘĄQ€€‚€‚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+Ë2Ě( €€˜˜‚Q€ ‚˙ ÜĚRÎD 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 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 andĎ2Ěa4 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 discRÎaíĘover the source code of the software or create derivative works from the software1RΒ1ą˙˙˙˙˙˙˙˙˙˙˙˙’é°a{9 @€a€†ŘĄQ€€‚€‚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€ ‚˙ß{ť6 :€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.Ś) "€\€†ŘĄQ€‚˙steam table calculations are not available.1ťC1Ž˙˙˙˙˙˙˙˙˙˙˙˙C é°,9 @€a€†ŘĄQ€€‚€‚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+CW( €€˜˜‚Q€ ‚˙I, 9 @€!€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Temperature - PressureThis subsection provides physical properties of the selected specie forassigned temperature and pressure.Input Values:Specie, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1WŃ1Ł˙˙˙˙˙˙˙˙ ˙˙˙˙ŃC íą ž< F€c€†ŘĄQ€€‚€‚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+Ńé( €€˜˜‚Q€ ‚˙ âž > 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:éC ) "€"€†ŘĄQ€‚˙the Main menu.1 t 1…˙˙˙˙˙˙˙˙ ˙˙˙˙t Č é°C ] 9 @€a€†ŘĄQ€€‚€‚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 ˆ ( €€˜˜‚Q€ ‚˙@] Č 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 constant1ˆ ů 1•˙˙˙˙˙˙˙˙ ˙˙˙˙ů i@é°Č â 9 @€a€†ŘĄQ€€‚€‚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+ů  ( €€˜˜‚Q€ ‚˙Ůâ /@= 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 /@Č  on the Exit button to go back to: i@) "€"€†ŘĄQ€‚˙the Main menu.1/@š@1€˙˙˙˙˙˙˙˙ ˙˙˙˙š@éBé°i@ƒA9 @€a€†ŘĄQ€€‚€‚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@ŽA( €€˜˜‚Q€ ‚˙;ƒAéB8 >€€†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 constant1ŽAC1’˙˙˙˙˙˙˙˙ ˙˙˙˙C{Fé°éBD9 @€a€†ŘĄQ€€‚€‚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+C.D( €€˜˜‚Q€ ‚˙ÖDAF= 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 physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:.D{F) "€"€†ŘĄQ€‚˙the Main menu.1AFŹF1~˙˙˙˙˙˙˙˙˙˙˙˙ŹFůJé°{F•G9 @€a€†ŘĄQ€€‚€‚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+ŹFŔG( €€˜˜‚Q€ ‚˙)ě•GéI= H€Ů€†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 [/]orS/R = A1*lnT + A2*T + A3*T^2/2 + A4*T^3/3 + A5*T^4/4âŔGůJ. *€Ĺ€†ŘĄQ€‚‚‚‚‚˙ + A7 - lnp [/]For each specie, two sets of coefficients are included for two adjecenttemperature intervals, 273 to 1,000 K and 1,000 to 5,000 K. The data havebeen constrained to be equal at 1,000 K.1éI*K1Š˙˙˙˙˙˙˙˙˙˙˙˙*K˘Mé°ůJL9 @€a€†ŘĄQ€€‚€‚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€ ‚˙d,L˘M8 >€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.1>LÓM1 ˙˙˙˙˙˙˙˙˙˙˙˙ÓMŻOé°˘MźN9 @€a€†ŘĄQ€€‚€‚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+ÓMçN( €€˜˜‚Q€ ‚˙ȘźNŻO0 .€1€†ŘĄQ€‚€‚‚‚˙Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1çNŕO1™˙˙˙˙˙˙˙˙˙˙˙˙ŕOť‚é°ŻOՀ9 @€a€†ŕOՀŻOŘĄQ€€‚€‚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+ŕO( €€˜˜‚Q€ ‚˙ťƒՀť‚8 >€€†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 Properties1ě‚1ˆ˙˙˙˙˙˙˙˙˙˙˙˙ě‚C†é°ť‚Ճ9 @€a€†ŘĄQ€€‚€‚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+ě‚„( €€˜˜‚Q€ ‚˙ ĚՃ †= 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:„C†) "€"€†ŘĄQ€‚˙the Main menu.1 †t†1U˙˙˙˙˙˙˙˙˙˙˙˙t†˜‰é°C†]‡9 @€a€†ŘĄQ€€‚€‚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†ˆ‡( €€˜˜‚Q€ ‚˙Ň]‡˜‰> 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.1ˆ‡ɉ1§˙˙˙˙˙˙˙˙˙˙˙˙ɉ?Œ鰘‰˛Š9 @€a€†ŘĄQ€€‚€‚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+ɉ݊( €€˜˜‚Q€ ‚˙b,˛Š?Œ6 :€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 Properties1݊pŒ1W˙˙˙˙˙˙˙˙˙˙˙˙pŒ–é°?ŒY9 @€a€†ŘĄQ€€‚€‚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+pŒ„( €€˜˜‚Q€ ‚˙ŐY–= 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.1„Ǐ1‰˙˙˙˙˙˙˙˙˙˙˙˙ǏŤÁ鰖źŔ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙ǏźŔ–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+ǏçŔ( €€˜˜‚Q€ ‚˙ĔźŔŤÁ0 .€)€†ŘĄQ€‚€‚‚‚˙Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1çŔÜÁ1Ě˙˙˙˙˙˙˙˙˙˙˙˙ÜÁwÄé°ŤÁĹÂ9 @€a€†ŘĄQ€€‚€‚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+ÜÁđÂ( €€˜˜‚Q€ ‚˙‡NĹÂwÄ9 @€€†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.1đ¨Ä1N˙˙˙˙˙˙˙˙˙˙˙˙¨ÄĹÇé°wÄ‘Ĺ9 @€a€†ŘĄQ€€‚€‚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+¨ÄźĹ( €€˜˜‚Q€ ‚˙ Ě‘ĹĹÇ= H€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - 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.1źĹöÇ1ţ˙˙˙˙˙˙˙˙˙˙˙˙öÇĂÉé°ĹÇßČ9 @€a€†ŘĄQ€€‚€‚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+öÇ É( €€˜˜‚Q€ ‚˙š‰ßČĂÉ0 .€€†ŘĄQ€‚€‚‚‚˙Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1 ÉôÉ1˙˙˙˙˙˙˙˙˙˙˙˙ôÉÇÍé°ĂÉÝĘ9 @€a€†ŘĄQ€€‚€‚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+ôÉË( €€˜˜‚Q€ ‚˙ŰÝĘÍ; 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.ŠËÇÍ* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1ÍřÍ1…˙˙˙˙˙˙˙˙˙˙˙˙řÍ<é°ÇÍáÎ9 @€a€†ŘĄQ€€‚€‚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+řÍ Ď( €€˜˜‚Q€ ‚˙@áÎX? 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 temp ĎXÇÍerature 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 defaultäŤ Ď<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.1Xm1\˙˙˙˙˙˙˙˙˙˙˙˙m˜é°<V9 @€a€†ŘĄQ€€‚€‚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+m( €€˜˜‚Q€ ‚˙ŰV•9 @€ˇ€†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 HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateՁ˜. *€Ť€†ŘĄQ€‚‚‚‚‚˙Assumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1•É1î˙˙˙˙˙˙˙˙˙˙˙˙Ɇ鰘˛9 @€a€†ŘĄQ€€‚€‚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+ÉÝ( €€˜˜‚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 defaultAÝ] < F€ €†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 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)÷ †2 2€ď€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙efficiency 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.1] ˇ1í˙˙˙˙˙˙˙˙˙˙˙˙ˇŤB鰆 9 @€a€†ŘĄQ€€‚€‚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+ˇË( €€˜˜‚Q€ ‚˙9ý B< F€ű€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚ËB†‚‚‚‚‚‚˙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›qËŤB* $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1BÜB1n˙˙˙˙˙˙˙˙˙˙˙˙ÜBHé°ŤBĹC9 @€a€†ŘĄQ€€‚€ ‚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+ÜBđC( €€˜˜‚Q€ ‚˙EĹC5F? 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 defaultäŤđCH9 @€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.15FJH1o˙˙˙˙˙˙˙˙ ˙˙˙˙JHˆLé°H3I9 @€a€†ŘĄQ€€‚€‚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+JH^I( €€˜˜‚Q€ ‚˙I 3I§K< F€€†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 HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.áś^IˆL+ $€m€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1§KšL1ö˙˙˙˙˙˙˙˙!˙˙˙˙šL„ƒ鰈L˘M9 @€a€†ŘĄQ€€‚€ ‚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+šLÍM( €€˜˜‚Q€ ‚˙D˘M€? 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 wÍM€ˆLith the defaultAÍM^‚< F€ €†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 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&ő€„ƒ1 0€ë€†ŘĄQ€‚‚‚‚‚‚‚‚˙efficiency 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.1^‚ľƒ1Ú˙˙˙˙˙˙˙˙"˙˙˙˙ľƒ^†鰄ƒž„9 @€a€†ŘĄQ€€‚€ ‚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+ľƒɄ( €€˜˜‚Q€ ‚˙•[ž„^†: 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.1Ʉ†1â˙˙˙˙˙˙˙˙#˙˙˙˙†@Šé°^†x‡9 @€a€†ŘĄQ€€‚€ ‚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+†Ł‡( €€˜˜‚Q€ ‚˙Óx‡˛‰< 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.ŽbŁ‡@Š, (€Ä€†ŘĄQ€‚‚‚‚˙STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1˛‰qŠ1Ů˙˙˙˙˙˙˙˙$˙˙˙˙qŠŽé°@ŠZ‹9 @€a€†ŘĄQ€€‚€ ‚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+qŠ…‹( €€˜˜‚Q€‚˙*ńZ‹Ż9 @€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?…‹Ž+ &€~€†ŘĄQ€‚‚‚˙Assumptions:Specific heat is constant. Four stroke engine.1ŻJŽ1 ˙˙˙˙˙˙˙˙%˙˙˙˙JŽÚÄé°Ž39 @€a€†ŘĄQ€€‚€ ‚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+JŽ^( €€˜˜‚Q€ ‚˙)ę3“Á? L€Ő€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: OttoSTEP 1Select the desired specie (working fluid) or go with the ^“ÁŽdefault 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!ĺ^´Ă< 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&ô“ÁÚÄ2 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.1´Ă Ĺ1ď˙˙˙˙˙˙˙˙&˙˙˙˙ ĹÉČé°ÚÄôĹ9 @€a€†ŘĄQ€€‚€ ‚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+ ĹĆ( €€˜˜‚Q€ ‚˙2ůôĹQČ9 @€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, FuelxLĆÉČ, (€˜€†ŘĄQ€‚‚‚‚˙ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1QČúČ1Ë˙˙˙˙˙˙˙˙'˙˙˙˙úČ”Ďé°ÉČăÉ9 @€a€†ŘĄQ€€‚€ ‚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+úČĘ( €€˜˜‚Q€ ‚˙/đăÉ=Ě? 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,đĘiÎ< 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+ů=Ě”Ď2 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.1iÎĹĎ1á˙˙˙˙˙˙˙˙(˙˙˙˙ĹĎ鰔Ďş9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙EĹĎş”Ďngineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĹĎĺ( €€˜˜‚Q€ ‚˙%ěş 9 @€Ů€†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 LengthOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Outlet Static Temperature,Outlet Static Pressure, Outlet Mach Number, Outlet StagnationůĘĺ/ ,€•€†ŘĄQ€‚‚‚‚‚‚˙Temperature, Outlet Stagnation Pressure, Enthalpy Extraction,Specific Work OutputAssumptions:Specific heat, velocity, conductivity, induced voltage field andmagnetic field strength are constant.1 41ü˙˙˙˙˙˙˙˙)˙˙˙˙4˙ é°9 @€a€†ŘĄQ€€‚€ ‚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+4H( €€˜˜‚Q€ ‚˙4ö|> 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.F H < 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 9Click on the Calculate button to start the calculation of the Magnetohydrodynamics cycle output values for the chosen input values.STEP 10When done with Steps 1 through 9, click on the Exit button to go back=|˙ ) "€(€†ŘĄQ€‚˙to the Main menu.1 0 1Ŕ˙˙˙˙˙˙˙˙*˙˙˙˙0 ż é°˙  9 @€a€†ŘĄQ€€‚€ ‚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 D ( €€˜˜‚Q€ ‚˙ß R / ,€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:mDD ż ) "€ˆ€†ŘĄQ€‚˙Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1R đ 1˙˙˙˙˙˙˙˙+˙˙˙˙đ XAé°ż Ů 9 @€a€†ŘĄQ€€‚€ ‚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 ( €€˜˜‚Q€ ‚˙ áŮ 0@? 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 temper0@ż ature value or go with the default(öXA2 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.10@‰A1˙˙˙˙˙˙˙˙,˙˙˙˙‰AuCé°XArB9 @€a€†ŘĄQ€€‚€ ‚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B( €€˜˜‚Q€ ‚˙بrBuC0 .€Q€†ŘĄQ€‚€‚‚‚˙Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1BŚC1Ř˙˙˙˙˙˙˙˙-˙˙˙˙ŚCMEé°uCD9 @€a€†ŘĄQ€€‚€ ‚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+ŚCşD( €€˜˜‚Q€ ‚˙“eDME. ,€Ę€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1şD~E1ň˙˙˙˙˙˙˙˙.˙˙˙˙~E?Hé°MEgF9 @€a€†ŘĄQ€€‚€ ‚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+~E’F( €€˜˜‚Q€ ‚˙­pgF?H= 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’FpH1Ö˙˙˙˙˙˙˙˙/˙˙˙˙pHMé°?HYI9 @€a€†ŘĄQ€€‚€ ‚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+pH„I( €€˜˜‚Q€ ‚˙ ÇYIKB 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 5ˆU„IM3 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KFM1˙˙˙˙˙˙˙˙0˙˙˙˙FM5€é°M/N9 @€a€†ŘĄQ€€‚€ ‚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+FMZN( €€˜˜‚Q€ ‚˙Ď‘/N5€> J€#€†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 Pressure, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic cZN5€Mompression. Specific heat is constant.1ZNf€1W˙˙˙˙˙˙˙˙1˙˙˙˙f€Œ…é°5€O9 @€a€†ŘĄQ€€‚€ ‚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+f€z( €€˜˜‚Q€ ‚˙ĆO‚ƒB 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 5 ÔzŒ…6 :€Š€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Enter 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‚ƒ˝…1Ő˙˙˙˙˙˙˙˙2˙˙˙˙˝…aˆ鰌…Ś†9 @€a€†ŘĄQ€€‚€ ‚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+˝…ц( €€˜˜‚Q€ ‚˙SŚ†aˆ= 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 compression1ц’ˆ1ž˙˙˙˙˙˙˙˙3˙˙˙˙’ˆ˙Œé°aˆ{‰9 @€a€†ŘĄQ€€‚€ ‚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+’ˆŚ‰( €€˜˜‚Q€ ‚˙Aţ{‰ç‹C T€ý€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power 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 default榉˙Œ2 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.1ç‹01Ö˙˙˙˙˙˙˙˙4˙˙˙˙0Վé°˙ŒŽ9 @€a€†ŘĄQ€€‚€ ‚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DŽ( €€˜˜‚Q€ ‚˙‘cŽՎ. ,€Ć€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1DŽ1Ş˙˙˙˙˙˙˙˙5˙˙˙˙™Âé°ŐŽ Ŕ9 @€a€†ŘĄQ€€‚€ ‚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 ŔՎ+7Ŕ( €€˜˜‚Q€ ‚˙Ů ŔOÂ? 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!7Ŕ™Â) "€B€†ŘĄQ€‚˙Specific heat is not constant.1OÂĘÂ1˙˙˙˙˙˙˙˙6˙˙˙˙ĘÂÉ鰙ÂłĂ9 @€a€†ŘĄQ€€‚€ ‚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+ĘÂŢĂ( €€˜˜‚Q€ ‚˙BłĂ Ć< 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.%ëŢĂEČ: 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 gasÓŚ ĆÉ- (€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.1EČIÉ1š˙˙˙˙˙˙˙˙7˙˙˙˙IɲĚé°É2Ę9 @€a€†ŘĄQ€€‚€ ‚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+IÉ]Ę( €€˜˜‚Q€ ‚˙ Ě2ĘhĚ? 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!]ʲĚ) "€B€†ŘĄQ€‚˙Specific heat is not constant.1hĚăĚ1v˙˙˙˙˙˙˙˙8˙˙˙˙ăĚ4é°˛ĚĚÍ9 @€a€†ŘĄQ€€‚€ ‚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+ăĚ÷Í( €€˜˜‚Q€ ‚˙7úĚÍ:= 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 t÷Í:˛Ěo normalize the oxidant composition for you.%ë÷Í_: 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§:4. *€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.1_e1Ô˙˙˙˙˙˙˙˙9˙˙˙˙eé°4N9 @€a€†ŘĄQ€€‚€ ‚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+ey( €€˜˜‚Q€ ‚˙aN. ,€Â€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1y91í˙˙˙˙˙˙˙˙:˙˙˙˙9őé°"9 @€a€†ŘĄQ€€‚€ ‚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+9M( €€˜˜‚Q€ ‚˙¨k"ő= 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.1M&1˙˙˙˙˙˙˙˙;˙˙˙˙&ř é°ő 9 @€a€†ŘĄQ€€‚€ ‚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€ ‚˙ß Y @ N€ż€†ŘĄQ€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Expansion: Isentropic (Ideal)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.Ÿj: ř 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.1Y ) 1 ˙˙˙˙˙˙˙˙<˙˙˙˙) @é°ř 9 @€a€†ŘĄQ€€‚€ ‚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€ ‚˙Ĺˆ@= H€€†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 Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant=@ř .1=?@1ť˙˙˙˙˙˙˙˙=˙˙˙˙?@ÉEé°@(A9 @€a€†ŘĄQ€€‚€ ‚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+?@SA( €€˜˜‚Q€ ‚˙Ţ(AqC@ 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. čSA‘E8 >€Ń€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 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 to8qCÉE( € €†ŘĄQ€˙the Main menu.1‘EúE1‘˙˙˙˙˙˙˙˙>˙˙˙˙úEZHé°ÉEăF9 @€a€†ŘĄQ€€‚€ ‚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+úEG( €€˜˜‚Q€ ‚˙LăFZH; 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 expansion1G‹H1˙˙˙˙˙˙˙˙?˙˙˙˙‹HçLé°ZHtI9 @€a€†ŘĄQ€€‚€ ‚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+‹HŸI( €€˜˜‚Q€ ‚˙3đtIŇKC 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 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 defaultăŸIçL2 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.1ŇKM1K˙˙˙˙˙˙˙˙@˙˙˙˙M>€é°çLN9 @€a€†ŘĄQ€€‚€ ‚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+M,N( €€˜˜‚Q€ ‚˙ËN>€; 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 Temperatur,N>€çLeAssumptions:Ideal heat transfer -- no losses1,No€1Ú˙˙˙˙˙˙˙˙A˙˙˙˙o€†é°>€X9 @€a€†ŘĄQ€€‚€ ‚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€ƒ( €€˜˜‚Q€ ‚˙ßXĄƒ? 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.=ƒޅ< 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:Ąƒ†) "€"€†ŘĄQ€‚˙the Main menu.1ޅI†1˙˙˙˙˙˙˙˙B˙˙˙˙I† ‰é°†2‡9 @€a€†ŘĄQ€€‚€ ‚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+I†]‡( €€˜˜‚Q€ ‚˙É2‡ ‰: 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]‡Q‰1W˙˙˙˙˙˙˙˙C˙˙˙˙Q‰wŽé° ‰:Š9 @€a€†ŘĄQ€€‚€ ‚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‰eŠ( €€˜˜‚Q€ ‚˙Ô:ŠwŒ> J€Š€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/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 theĆeŠwŽ: 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.1wŒ¨Ž1Ă˙˙˙˙˙˙˙˙D˙˙˙˙¨ŽAŔé°wŽ‘9 @€a€†ŘĄQ€€‚€ ‚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+¨Žź( €€˜˜‚Q€ ‚˙yK‘AŔ. ,€–€†ŘĄQ€‚€‚‚˙Compressible FlowTźAŔwŽhis section provides analysis of compressible flow.1źrŔ1P˙˙˙˙˙˙˙˙E˙˙˙˙rŔ‘Âé°AŔ[Á9 @€a€†ŘĄQ€€‚€ ‚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+rŔ†Á( €€˜˜‚Q€ ‚˙ Ó[Á‘Â8 >€§€†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 constant1†ÁÂÂ13˙˙˙˙˙˙˙˙F˙˙˙˙ÂÂÄĹ鰑ÂŤĂ9 @€a€†ŘĄQ€€‚€ ‚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+ÂÂÖĂ( €€˜˜‚Q€ ‚˙ĂÄĹ< 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.1ÖĂőĹ1K˙˙˙˙˙˙˙˙G˙˙˙˙őĹČé°ÄĹŢĆ9 @€a€†ŘĄQ€€‚€ ‚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+őĹ Ç( €€˜˜‚Q€ ‚˙ÎŢĆČ8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1 Ç@Č1¤˙˙˙˙˙˙˙˙H˙˙˙˙@ČłËé°Č)É9 @€a€†ŘĄQ€€‚€ ‚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+@ČTÉ( €€˜˜‚Q€ ‚˙%ç)ÉyË> 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.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:TÉłË) "€"€†ŘĄQ€‚˙the Main menu.1yËäË1˙˙˙˙˙˙˙˙I˙˙˙˙äËłÍé°łËÍĚ9 @€a€†ŘĄQ€€‚€ ‚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+äËřĚ( €€˜˜‚Q€ ‚˙ť‹ÍĚłÍ0 .€€†ŘĄQ€‚€‚‚‚˙Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1řĚäÍ1“˙˙˙˙˙˙˙˙J˙˙˙˙äÍGé°łÍÍÎ9 @€a€†ŘĄQ€€‚€ ‚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+äÍřÎ( €€˜˜‚Q€ ‚˙C ÍÎG8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Properties: StagnationThis subsection provides analysis of stagnation properties.Input Values:Working Fluid, Static Temperature, VelocityOutput Values:Stagnation Temperature, StřÎGłÍagnation PressureAssumptions:Specific heat is constant1řÎx1G˙˙˙˙˙˙˙˙K˙˙˙˙xŽé°Ga9 @€a€†ŘĄQ€€‚€ ‚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+xŒ( €€˜˜‚Q€ ‚˙*ęaś@ 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 stagnationŘŞŒŽ. *€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.1śż1|˙˙˙˙˙˙˙˙L˙˙˙˙ż 鰎¨9 @€a€†ŘĄQ€€‚€ ‚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+żÓ( €€˜˜‚Q€ ‚˙7˙¨ 8 >€˙€†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 constant1Ó;1I˙˙˙˙˙˙˙˙M˙˙˙˙;S é° $9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+;O( €€˜˜‚Q€ ‚˙0ň$ > 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 staticÔŚOS . *€M€†ŘĄQ€‚‚‚‚‚˙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.1 „ 1†˙˙˙˙˙˙˙˙N˙˙˙˙„ Ů é°S m 9 @€a€†ŘĄQ€€‚€ ‚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€ ‚˙A m Ů 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 constant1˜  1i˙˙˙˙˙˙˙˙O˙˙˙˙ 7Bé°Ů ó9 @€a€†ŘĄQ€€‚€ ‚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€ ‚˙)ëóSA> J€×€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: NozzleSTEP 1Select the desired working fluid (specie) or go with the default value.STEP 2Enter the desired stagnation temperSAŮ ature 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,äľ7B/ ,€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.1SAhB1K˙˙˙˙˙˙˙˙P˙˙˙˙hB‚Eé°7BQC9 @€a€†ŘĄQ€€‚€ ‚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+hB|C( €€˜˜‚Q€ ‚˙ĘQC‚E< 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 constant1|CłE1ß˙˙˙˙˙˙˙˙Q˙˙˙˙łEaJ鰂EœF9 @€a€†ŘĄQ€€‚€ ‚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+łEÇF( €€˜˜‚Q€ ‚˙ ĚœFŃH> 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_ÇFaJ1 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.1ŃH’J1Š˙˙˙˙˙˙˙˙R˙˙˙˙’JëLé°aJ{K9 @€a€†ŘĄQ€€‚€ ‚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+’JŚK( €€˜˜‚Q€ ‚˙E {KëL8 >€€†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 constant1ŚKM1_˙˙˙˙˙˙˙˙S˙˙˙˙M;é°ëLN9 @€a€†ŘĄQ€€‚€ ‚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+M0N( €€˜˜‚Q€ ‚˙ÝNW€> 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.STEP0NW€ëL 5Click on the Calculate button to start the calculation of Mach number,äľ0N;/ ,€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.1W€l1ż˙˙˙˙˙˙˙˙T˙˙˙˙lúƒé°;U‚9 @€a€†ŘĄQ€€‚€ ‚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+l€‚( €€˜˜‚Q€ ‚˙zAU‚úƒ9 @€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 constant1€‚+„1˙˙˙˙˙˙˙˙U˙˙˙˙+„‰é°úƒ…9 @€a€†ŘĄQ€€‚€ ‚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€ ‚˙.đ…m‡> 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§p?…‰7 <€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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