?_o˙˙˙˙ ¤_Vlţ„ € ‰€ ‚˙Temperature - Pressure\+ƒ/1 2€V€€ƒƒăŒ€ ‰€ ‚˙Running - Temperature - PressureMÓ|2 4€6€°˜€ƒă? € ‰€ ‚˙Enthalpy - PressureY(/Ő1 2€P€€ ƒƒăˇ€ ‰€ ‚˙Running - Enthalpy - PressureL|!2 4€4€°˜€ƒă@ € ‰€ ‚˙Entropy - PressureX'Őy1 2€N€€ƒƒă⍀ ‰€ ‚˙Running - Entropy - Pressure@!š. ,€$€°˜ă€‰€‚˙Power Cycles@yů2 4€€˜˜€ƒă°€ ‰€ ‚˙CarnotR!šK1 2€B€€ƒƒă˛ú€ ‰€ ‚˙Running - Carnot CycleAůŒ2 4€€°˜€ƒăą€ ‰€ ‚˙BraytonIKŐ3 6€,€˜˜€ƒƒănŤ€ ‰€ ‚˙Power (Ideal)e3Œ:2 4€f€€ƒƒƒăœGž€ ‰€ ‚˙Running - Brayton Cycle: Power (Ideal)HŐ‚3 6€*€°˜€ƒƒăoŤ€ ‰€ ‚˙Power (Real)d2:ć2 4€d€€ ƒƒƒăÇGž€ ‰€ ‚˙Running - Brayton Cycle: Power (Real)J‚00 0€4€°˜€ ƒƒăpŤ‰€ ‚˙Propulsion (Ideal)j8ćš2 4€p€€ ƒƒƒăňGž€ ‰€ ‚˙Running - Brayton Cycle: Propulsion (Ideal)I0ă0 0€2€°˜€ ƒƒăqŤ‰€ ‚˙Propulsion (Real)i7šL2 4€n€€ ƒƒƒăHž€ ‰€ ‚˙Running - Brayton Cycle: Propulsion (Real)T&ă . ,€L€°˜ă€‰€‚˙Power Cycle Components/Processesm,L A R€X€˜˜€ƒăé€ ‰€ ‚€ ƒƒăćB߉€ ‚˙CompressionIsentropic (Ideal)h6 u 2 4€l€€ ƒƒƒăÄ<€%€ ‰€ ‚˙Running - Compression: Isentropic (Ideal)I ž 0 0€2€°˜€ ƒƒăçB߉€ ‚˙Isentropic (Real)g5u % 2 4€j€€ ƒƒƒăď<€%€ ‰€ ‚˙Running - Compression: Isentropic (Real)Bž g 0 0€$€°˜€ ƒƒăčB߉€ ‚˙Isothermal`.% Ç 2 4€\€€ ƒƒƒă=€%€ ‰€ ‚˙Running - Compression: Isothermal@g  / .€"€°˜€ ƒăꉀ ‚˙Combustion@Ç G 0 0€ €˜˜€ ƒƒăJ߉€ ‚˙Coal/Oil]+ ¤ 2 4€V€€ ƒƒƒăWs%€ ‰€ ‚˙Running - Combustion: Coal/Oil; G ß 0 0€€°˜€ ƒƒă J߉€ ‚˙GasX&¤ 7 2 4€L€€ ƒƒƒă‚s%€ ‰€ ‚˙Running - Combustion: Gas?ß v / .€ €°˜€ ƒă뉀 ‚˙ExpansionJ7 Ŕ 0 0€4€˜˜€ ƒƒăXQ߉€ ‚˙Isentropic (Ideal)f4v & 2 4€h€€ ƒƒƒăꩂ%€ ‰€ ‚˙Running - Expansion: Isentropic (Ideal)IŔ o 0 0€2€°˜€ ƒƒăYQ߉€ ‚˙Isentropic (Real)e3& Ô 2 4€f€€ ƒƒƒăŞ‚%€ ‰€ ‚˙Running - Expansion: Isentropic (Real)Bo 0 0€$€°˜€ ƒƒăZQ߉€ ‚˙Isothermal^,Ô t2 4€X€€ ƒƒƒă@Ş‚%€ ‰€ ‚˙Running - Expansion: IsothermalEš. ,€.€°˜ă€‰€‚˙Compressible FlowGt/ .€0€˜˜€ ƒă"&‰€ ‚˙Velocity of SoundW&šW1 2€L€€ ƒƒăŘg€ ‰€ ‚˙Running - Velocity of SoundA˜/ .€$€°˜€ ƒă#&‰€ ‚˙Mach NumberQ W @1 2€@€€ ƒƒăh€ ‰€ ‚˙Running - Mach Number˜ @ @˜L@/ .€"€°˜€ ƒă$&‰€ ‚˙PropertiesB @Ž@0 0€$€˜˜€ ƒƒă |‰€ ‚˙Stagnation]+L@ë@2 4€V€€ ƒƒƒăĽŐE.€ ‰€ ‚˙Running - Stagnation Properties>Ž@)A0 0€€°˜€ ƒƒă |‰€ ‚˙StaticY'ë@‚A2 4€N€€ ƒƒƒăĐŐE.€ ‰€ ‚˙Running - Static Properties< )AžA/ .€€°˜€ ƒă%&‰€ ‚˙NozzleL‚A B1 2€6€€ ƒƒăYh€ ‰€ ‚˙Running - NozzleBžALB/ .€&€°˜€ ƒă&&‰€ ‚˙Normal ShockR! BžB1 2€B€€ ƒƒă„h€ ‰€ ‚˙Running - Normal Shock>LBÜB/ .€€°˜€ ƒă'&‰€ ‚˙DiffuserNžB*C1 2€:€€ ƒƒăŻh€ ‰€ ‚˙Running - Diffuser< ÜBfC/ .€€°˜€ ƒă(&‰€ ‚˙ThrustL*C˛C1 2€6€€ ƒƒăÚh€ ‰€ ‚˙Running - Thrust1fCăC17 ˙˙˙˙˙˙˙˙˙˙˙˙ăCéM빲CÎD: 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+ăCůD( €€˜˜‚Q€ ‚˙G ÎD@G= H€€€‚€‚€ €‚€ €‚‚‚‚‚‚‚‚˙Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Gas Dynamics, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, analyzes power cycles, power cycle components/processesand compressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofpower and propulsion systems. It should provide you with the opportunity×ůDXIA P€Ż€€‚‚‚‚‚€ €€ €‚‚€ ‚€ƒ‚ƒ‚˙to more quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outmore about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (301) 540-3605.Thermodynamic and Transport PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and Pressure Ś@GaKc ”€M€€ƒ‚‚€ ‚€ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚˙Entropy and PressurePower CyclesCarnotBrayton (Power and Propulsion)Power Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowVelocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard drive?XI K$ €6€€ƒ‚˙IBM compatible systems:h:aKL. ,€t€†üEĄ€ƒƒ‚ƒƒ‚˙Windows 98, Windows 2000, Windows ME andWindows XP ß KM, &€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.ÖĽLéM1 0€K€€‚€ ‚€‚‚‚‚‚‚˙Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1MN1q˙˙˙˙˙˙˙˙˙˙˙˙Nf…ëąéMO: 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+N0O( €€˜˜‚Q€ ‚˙ ËOE> J€—€†ŘĄQ€‚€‚€ €‚‚‚‚‚‚‚‚‚‚˙Claim SheetEngineering Software products allow quick and reliablecalculation of thermodynamic and transport properties ofgaseous, liquid a0OEéMnd 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:"ŕ0OgƒB 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˙ˇEf…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 constant1gƒ—…17˙˙˙˙˙˙˙˙˙˙˙˙—…ˆëąf…‚†: 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€ ‚˙𾂆ˆ; D€k€†ŘĄQ€‚€‚€ €‚‚‚‚‚‚‚˙How to Use the ProgramIn each section, subsection of the Gas Dynamics program, the userneeds to change one or more input values in order to calculate a newcase. Input values are in boxes with white background and can bechanged by clicking on each individual box or even by using the arrowkeys and changing the current value. Output values cannot bemodified, changed by the user and they are in boxes with blackbackground.1­†Îˆ1W˙˙˙˙˙˙˙˙˙˙˙˙ΈôŽëąˆš‰: 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+Έä‰( €€˜˜‚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 thisAńä‰ZŽP 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, thenšmŒôŽ- *€Ú€†ŘĄQ€ €‚‚˙Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1ZŽ%1˙˙˙˙˙˙˙˙˙˙˙˙%ĂëąôŽŔ: 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.engi%ŔôŽneering-4e.com+%GŔ( €€˜˜‚Q€ ‚˙LŔ“Ŕ- *€>€†ŘĄQ€‚€‚˙Suggestion/Evaluation FormÜGŔ§Á8 >€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‘]“Ŕ8Â4 8€ş€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:8§ÁpÂ) "€€ †ŘĄQ€ ‚˙Gas Dynamics—Z8ÂĂ= J€´€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Quality:Usefulness:Possible areas of improvement:Other suggestions:1pÂ8Ă1j˙˙˙˙˙˙˙˙˙˙˙˙8ĂqČëąĂ#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+8ĂNÄ( €€˜˜‚Q€ ‚˙ Ü#ÄnĆD 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 andĎNÄqČ4 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 software1nƢČ1ł˙˙˙˙˙˙˙˙˙˙˙˙˘Č$ĚëąqȍÉ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+˘Č¸É( €€˜˜‚Q€ ‚˙ߍÉÍË6 :€ż€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚˙PropertiesThis section provides physical properties of available species forassigned two state values such as: temperature and pressure,enthalpy and pressure, and entropy and pressure. Physical propertiesare given in both U.S. customary and International units.Note: Physical properties for H2O(S), H2O(L) and H2O(G) areavailable. The accuracy of the available H2O properties is only goodfor the purpose of combustion calculation. Therefore, this indicates thatW.¸É$Ě) "€\€†ŘĄQ€‚˙steam table calculations are not available.1ÍËUĚ1˙˙˙˙˙˙˙˙˙˙˙˙UĚ´Îëą$Ě@Í: 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+UĚkÍ( €€˜˜‚Q€ ‚˙I@Í´Î9 @€!€†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 constant1kÍĺÎ1}˙˙˙˙˙˙˙˙ ˙˙˙˙ĺÎfﲴÎÔĎ= 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+ĺÎ ( €€˜˜‚Q€ ‚˙ÔĎ ´Î âÔĎ,> 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: f) "€"€†ŘĄQ€‚˙the Main menu.1,—1‡˙˙˙˙˙˙˙˙ ˙˙˙˙—íëąf‚: 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€ ‚˙@‚í9 @€€†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 constant1­1—˙˙˙˙˙˙˙˙ ˙˙˙˙„ëąí : 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 J= 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:4„) "€"€†ŘĄQ€‚˙the Main menu.1Jľ1‚˙˙˙˙˙˙˙˙ ˙˙˙˙ľ 뱄  : 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+ľË ( €€˜˜‚Q€ ‚˙;   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 constant1Ë 7 1”˙˙˙˙˙˙˙˙ ˙˙˙˙7 šëą " : 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+7 M ( €€˜˜‚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 physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:M š) "€"€†ŘĄQ€‚˙the Main menu.1`Ë1ç˙˙˙˙˙˙˙˙˙˙˙˙ËľB뱚ś: 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+Ëá( €€˜˜‚Q€ ‚˙(íśB; D€Ű€áBš†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 váľB* $€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.1BćB1Ť˙˙˙˙˙˙˙˙˙˙˙˙ćB`EëąľBŃC: 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+ćBüC( €€˜˜‚Q€ ‚˙d,ŃC`E8 >€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.1üC‘E1˙˙˙˙˙˙˙˙˙˙˙˙‘EoGëą`E|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+‘E§F( €€˜˜‚Q€ ‚˙Ș|FoG0 .€1€†ŘĄQ€‚€‚‚‚˙Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1§F G1˙˙˙˙˙˙˙˙˙˙˙˙ GqJëąoG‹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+ GśH( €€˜˜‚Q€ ‚˙ťƒ‹HqJ8 >€€†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 Properties1śH˘J1Š˙˙˙˙˙˙˙˙˙˙˙˙˘JűMëąqJK: 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+˘J¸K( €€˜˜‚Q€ ‚˙ ̍KÁM= 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:¸KűM) "€"€†ŘĄQ€‚˙the Main menu.1ÁM,N1x˙˙˙˙˙˙˙˙˙˙˙˙,N^ëąűMO: 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+,NBO( €€˜˜‚Q€ ‚˙ŇO^> J€Ľ€†ŘĄQ€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Steam Approximations:Saturated Area: Pressure DependentSTEP 1Enter the desired saturated steam pressure valuBO^űMe 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.1BO1Š˙˙˙˙˙˙˙˙˙˙˙˙„ëą^z‚: 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+Ľ‚( €€˜˜‚Q€ ‚˙b,z‚„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 Properties1Ľ‚8„1Y˙˙˙˙˙˙˙˙˙˙˙˙8„`‡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+8„N…( €€˜˜‚Q€ ‚˙Ő#…`‡= 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.1N…‘‡1Ń˙˙˙˙˙˙˙˙˙˙˙˙‘‡1‰ëą`‡|ˆ: 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€ ‚˙Š\|ˆ1‰. ,€¸€†ŘĄQ€‚€‚‚˙Power CyclesThis section provides analysis of a few power cycles (Carnot and Brayton).1§ˆb‰1Î˙˙˙˙˙˙˙˙˙˙˙˙b‰˙‹ëą1‰MŠ: 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‰xŠ( €€˜˜‚Q€ ‚˙‡NMŠ˙‹9 @€€†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.1xŠ0Œ1P˙˙˙˙˙˙˙˙˙˙˙˙0ŒO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+0ŒF( €€˜˜‚Q€ ‚˙ ̍O= 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.1F€1:˙˙˙˙˙˙˙˙˙˙˙˙€[ÁëąOwŔ: B€c€†ŘĄQ€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(3€wŔO01) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+€˘Ŕ( €€˜˜‚Q€ ‚˙š‰wŔ[Á0 .€€†ŘĄQ€‚€‚‚‚˙Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1˘ŔŒÁ1˙˙˙˙˙˙˙˙˙˙˙˙ŒÁaĹëą[ÁwÂ: 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+ŒÁ˘Â( €€˜˜‚Q€ ‚˙Űw¸Ä; 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.Š˘ÂaĹ* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1¸Ä’Ĺ1k˙˙˙˙˙˙˙˙˙˙˙˙’ĹĚĘëąaĹ}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+’ŨĆ( €€˜˜‚Q€ ‚˙@}ĆčČ? 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 default䍨ĆĚĘ9 @€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.1čČýĘ1˙˙˙˙˙˙˙˙˙˙˙˙ýĘŃÎëąĚĘčË: 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+ýĘĚ( €€˜˜‚Q€ ‚˙ÚčË(Î; 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 RateAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.ŠĚŃÎ* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1(ÎĎ1k˙˙˙˙˙˙˙˙˙˙˙˙ĎZëąŃÎ : 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.comĎ ŃÎ+Ď7( €€˜˜‚Q€ ‚˙? v? 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 defaultäŤ7Z9 @€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.1v‹1˙˙˙˙˙˙˙˙˙˙˙˙‹uëąZv: 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+‹Ą( €€˜˜‚Q€ ‚˙9ývÚ< 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›qĄu* $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ÚŚ1p˙˙˙˙˙˙˙˙˙˙˙˙Śĺ ëąu‘ : 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+Śź ( €€˜˜‚Q€ ‚˙E‘  ? 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 default䍟 ĺ 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;˙˙˙˙˙˙˙˙ ˙˙˙˙ Bëąĺ : 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€ ‚˙8üpA< F€ů€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: Brayton: Propulsion (Real)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Work,pAĺ ing 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›q, B* $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1pA 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 ~ÉúÍ< 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 the chosen input values.d˛ËŠÎ, (€Č€†ŘĄQ€‚‚‚‚˙STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1úÍťÎ1q˙˙˙˙˙˙˙˙*˙˙˙˙ťÎX뱊ÎŚĎ: 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+ťÎŃĎ( €€˜˜‚Q€ ‚˙ߌĎë/ ,€ż€€‚€‚‚‚‚‚‚‚‚˙ŃĎëŠÎPower 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:mDŃĎX) "€ˆ€†ŘĄQ€‚˙Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1ë‰1˙˙˙˙˙˙˙˙+˙˙˙˙‰çëąXt: 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+‰Ÿ( €€˜˜‚Q€ ‚˙ átż? 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(öŸç2 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.1ż1˙˙˙˙˙˙˙˙,˙˙˙˙ďëąç: 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‘ď0 .€#€†ŘĄQ€‚€‚‚‚˙Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1. 1Ú˙˙˙˙˙˙˙˙-˙˙˙˙ É ëąď : 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+ 6 ( €€˜˜‚Q€ ‚˙“e É . ,€Ę€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.16 ú 1ô˙˙˙˙˙˙˙˙.˙˙˙˙ú ˝ ëąÉ ĺ : 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+ú  ( €€˜˜‚Q€ ‚˙­pĺ ˝ = 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 î 1Ú˙˙˙˙˙˙˙˙/˙˙˙˙î ĄAëą˝ Ů : 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 ( €€˜˜‚Q€ ‚˙ ÇŮ @B 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 val@˝ ue.STEP 5ˆUĄA3 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@ŇA1ó˙˙˙˙˙˙˙˙0˙˙˙˙ŇA”D빥A˝B: 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+ŇAčB( €€˜˜‚Q€ ‚˙Źo˝B”D= 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.1čBĹD1×˙˙˙˙˙˙˙˙1˙˙˙˙ĹDkI뱔D°E: 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+ĹDŰE( €€˜˜‚Q€ ‚˙ưEăGB 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 5ˆUŰEkI3 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.1ăGœI1×˙˙˙˙˙˙˙˙2˙˙˙˙œIBLëąkI‡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+œI˛J( €€˜˜‚Q€ ‚˙S‡JBL= 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 compression1˛JsL1R˙˙˙˙˙˙˙˙3˙˙˙˙sLî€ëąBL^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+sL‰M( €€˜˜‚Q€ ‚˙Aţ^MĘOC 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 defaultć‰Mî€2 2€Í€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙masĘOî€BLs 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.1ĘO1Ř˙˙˙˙˙˙˙˙4˙˙˙˙Ƃëąî€ ‚: 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+5‚( €€˜˜‚Q€ ‚˙‘c ‚Ƃ. ,€Ć€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.15‚÷‚1Š˙˙˙˙˙˙˙˙5˙˙˙˙÷‚o†ëąĆ‚âƒ: 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€ ‚˙Ůâƒ%†? 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! „o†) "€B€†ŘĄQ€‚˙Specific heat is not constant.1%† †1˙˙˙˙˙˙˙˙6˙˙˙˙ †đŒëąo†‹‡: 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€ ‚˙B‹‡ř‰< 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.%뜇Œ: 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 gasÓŚř‰đŒ- (€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.1Œ!1Ž˙˙˙˙˙˙˙˙7˙˙˙˙!˜ŔëąđŒ 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+!7Ž( €€˜˜‚Q€ ‚˙ Ě ŽNŔ? 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 CompositionAssump7ŽNŔđŒtions:Complete combustion. No gas dissociation. No heat loss.J!7Ž˜Ŕ) "€B€†ŘĄQ€‚˙Specific heat is not constant.1NŔÉŔ1x˙˙˙˙˙˙˙˙8˙˙˙˙ÉŔÇ빘Ŕ´Á: 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+ÉŔßÁ( €€˜˜‚Q€ ‚˙7ú´ÁÄ= 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.%ëßÁ;Ć: 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§ÄÇ. *€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;ĆAÇ1Ö˙˙˙˙˙˙˙˙9˙˙˙˙AÇćČëąÇ,Č: 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+AÇWČ( €€˜˜‚Q€ ‚˙a,ČćČ. ,€Â€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1WČÉ1ď˙˙˙˙˙˙˙˙:˙˙˙˙ÉŐËëąćČĘ: 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+É-Ę( €€˜˜‚Q€ ‚˙¨kĘŐË= 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.1-ĘĚ1Ż˙˙˙˙˙˙˙˙;˙˙˙˙ĚćëąŐËńĚ: 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+ĚÍ( €€˜˜‚Q€ ‚˙ßńĚ;Ď@ 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.ŸjÍć5 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 but;ĎćŐËton 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;Ď1î˙˙˙˙˙˙˙˙<˙˙˙˙Ôëąć: 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€ ‚˙§jÔ= 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.1-1˙˙˙˙˙˙˙˙=˙˙˙˙ŘëąÔđ: 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€ ‚˙Ţđ9@ 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.ŸjŘ5 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.19 1“˙˙˙˙˙˙˙˙>˙˙˙˙ k ëąŘô : 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€ ‚˙Lô k ; 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 expansion1 œ 1˙˙˙˙˙˙˙˙?˙˙˙˙œ  @ëąk ‡ : 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€ ‚˙3đ‡ ĺC 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 default㲠 @2 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.ĺ @k 1ĺ=@1M˙˙˙˙˙˙˙˙@˙˙˙˙=@YCëą @(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+=@SA( €€˜˜‚Q€ ‚˙Ë(AYC; 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 losses1SAŠC1Ü˙˙˙˙˙˙˙˙A˙˙˙˙ŠC5IëąYCuD: 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+ŠC D( €€˜˜‚Q€ ‚˙ßuDžF? 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.= DűH< 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:žF5I) "€"€†ŘĄQ€‚˙the Main menu.1űHfI1 ˙˙˙˙˙˙˙˙B˙˙˙˙fI?Lëą5IQJ: 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+fI|J( €€˜˜‚Q€ ‚˙ÉQJ?L: 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|JpL1ť˙˙˙˙˙˙˙˙C˙˙˙˙pL¤ëą?L[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+pL†M( €€˜˜‚Q€ ‚˙Ô[M˜O> 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 theƆM¤: B€€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙default temperature value.STEP 5Select the˜O¤?L 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.1˜OՁ1Ŕ˙˙˙˙˙˙˙˙D˙˙˙˙Ձdƒ빤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@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ձë‚( €€˜˜‚Q€ ‚˙yKŔ‚dƒ. ,€–€†ŘĄQ€‚€‚‚˙Compressible FlowThis section provides analysis of compressible flow.1ë‚•ƒ1R˙˙˙˙˙˙˙˙E˙˙˙˙•ƒś…ëądƒ€„: 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+•ƒŤ„( €€˜˜‚Q€ ‚˙ Ӏ„ś…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 constant1Ť„ç…15˙˙˙˙˙˙˙˙F˙˙˙˙ç…ëˆëąś…҆: 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+ç…ý†( €€˜˜‚Q€ ‚˙î˛҆ëˆ< 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.1ý†‰1M˙˙˙˙˙˙˙˙G˙˙˙˙‰8‹ëąëˆŠ: 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+‰2Š( €€˜˜‚Q€ ‚˙Ί8‹8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant12Ši‹1Ś˙˙˙˙˙˙˙˙H˙˙˙˙i‹ގëą8‹TŒ: 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+i‹Œ( €€˜˜‚Q€ ‚˙%çTŒ¤Ž> 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:Œގ) "€"€†ŘĄQ€‚˙the Main menu.1¤Ž1˙˙˙˙˙˙˙˙I˙˙˙˙ňŔëąŢŽ 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@engineering-4e.comWeb Site:http://www.engineering-4e.com Ŕގ+7Ŕ( €€˜˜‚Q€ ‚˙ť‹ ŔňŔ0 .€€†ŘĄQ€‚€‚‚‚˙Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.17Ŕ#Á1Š˙˙˙˙˙˙˙˙J˙˙˙˙#Á|ĂëąňŔÂ: 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+#Á9Â( €€˜˜‚Q€ ‚˙C Â|Ă8 >€€†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 constant19­Ă1I˙˙˙˙˙˙˙˙K˙˙˙˙­ĂĹÇëą|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+­ĂĂÄ( €€˜˜‚Q€ ‚˙*ę˜ÄíĆ@ 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 stagnationŘŞĂÄĹÇ. *€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.1íĆöÇ1~˙˙˙˙˙˙˙˙L˙˙˙˙öÇCĘëąĹÇáČ: 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+öÇ É( €€˜˜‚Q€ ‚˙7˙áČCĘ8 >€˙€†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 ÉtĘ1K˙˙˙˙˙˙˙˙M˙˙˙˙tĘŽÎëąCĘ_Ë: 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+tĘŠË( €€˜˜‚Q€ ‚˙0ň_ËşÍ> 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 staticÔŚŠËŽÎ. *€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.1şÍżÎ1b˙˙˙˙˙˙˙˙N˙˙˙˙żÎ"뱎ÎŞĎ: 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+żÎŐĎ( €€˜˜‚Q€ ‚˙A ŞĎ"8 >€€†ŘĄQ€‚€ŐĎ"ŽÎ‚‚‚‚‚‚‚‚‚‚‚˙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 constant1ŐĎS1T˙˙˙˙˙˙˙˙O˙˙˙˙Svëą">: 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+Si( €€˜˜‚Q€ ‚˙)ë>’> 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,äľiv/ ,€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.1’§1M˙˙˙˙˙˙˙˙P˙˙˙˙§Ăëąv’: 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€ ‚˙Ę’Ă< 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˝ô1á˙˙˙˙˙˙˙˙Q˙˙˙˙ô¤ ëąĂß : 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+ô ( €€˜˜‚Q€ ‚˙ Ěß  > 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_ ¤ 1 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 Ő 1Œ˙˙˙˙˙˙˙˙R˙˙˙˙Ő <@빤 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@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ő ë( €€˜˜‚Q€ ‚˙E Ŕ<@8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: DiffuserThis subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation Prë<@¤ essureAssumptions:Specific heat is constant1ëm@1F˙˙˙˙˙˙˙˙S˙˙˙˙m@‚Dëą<@XA: 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+m@ƒA( €€˜˜‚Q€ ‚˙ÝXAžC> 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,侃A‚D/ ,€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.1žCłD1Á˙˙˙˙˙˙˙˙T˙˙˙˙łDCG뱂DžE: 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+łDÉE( €€˜˜‚Q€ ‚˙zAžECG9 @€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 constant1ÉEtG1˙˙˙˙˙˙˙˙U˙˙˙˙tG_LëąCG_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+tGŠH( €€˜˜‚Q€ ‚˙.đ_H¸J> 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§pŠH_L7 <€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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