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Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com\7=‚% €n€°°€‚˙Power and Propulsion Systems Analysis 1.1 - TutorialHş&ĘŽ ę€u€˜˜ă\ŞÓP€‰€‚ăS?€‰€‚ă$çdI€‰€‚ăĚ˙§n€‰€‚ă\–€‰€‚ăf˘v´€‰€‚〉€‚€ƒă> € ‰€ ‚˙Program DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPropertiesTemperature - Pressure\+‚&1 2€V€€ƒƒăŒ€ ‰€ ‚˙Running - Temperature - PressureMĘs2 4€6€°˜€ƒă? € ‰€ ‚˙Enthalpy - PressureY(&Ě1 2€P€€ ƒƒăˇ€ ‰€ ‚˙Running - Enthalpy - PressureLs2 4€4€°˜€ƒă@ € ‰€ ‚˙Entropy - PressureX'Ěp1 2€N€€ƒƒă⍀ ‰€ ‚˙Running - Entropy - Pressure^Î? 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Ä 3 6€,€˜˜€ƒƒă5Ť€ ‰€ ‚˙Power (Ideal)d2{ ( 2 4€d€€ƒƒƒăUëÁ€ ‰€ ‚˙Running - Diesel Cycle: Power (Ideal)HÄ p 3 6€*€˜˜€ƒƒănŤ€ ‰€ ‚˙Power (Real)c1( Ó 2 4€b€€ƒƒƒă€ëÁ€ ‰€ ‚˙Running - Diesel Cycle: Power (Real)ŸQp r N l€˘€˜˜ă€‰€‚€ƒăé€ ‰€ ‚€ ƒƒăćB߉€ ‚˙Power Cycle Components/ProcessesCompressionIsentropic (Ideal)h6Ó Ú 2 4€l€€ ƒƒƒăÄ<€%€ ‰€ ‚˙Running - Compression: Isentropic (Ideal)Ir # 0 0€2€°˜€ ƒƒăçB߉€ ‚˙Isentropic (Real)g5Ú Š 2 4€j€€ ƒƒƒăď<€%€ ‰€ ‚˙Running - Compression: Isentropic (Real)B# Ě 0 0€$€°˜€ ƒƒăčB߉€ ‚˙Isothermal`.Š ,2 4€\€€ ƒƒƒă=€%€ ‰€ ‚˙Running - Compression: Isothermal@Ě l/ .€"€°˜€ ƒăꉀ ‚˙Combustion@,Ź0 0€ €˜˜€ ƒƒăJ߉€ ‚˙Coal/Oil]+l 2 4€V€€ ƒƒƒăWs%€ ‰€ ‚˙Running - Combustion: Coal/Oil; ŹD0 0€€°˜€ ƒƒă J߉€ ‚˙GasX& œ2 4€L€€ ƒƒƒă‚s%€ ‰€ ‚˙Running - Combustion: Gas?DŰ/ .€ €°˜€ ƒă뉀 ‚˙ExpansionJœ1@0 0€4€˜˜€ ƒƒŰ1@ ăXQ߉€ ‚˙Isentropic (Ideal)f4Ű—@2 4€h€€ ƒƒƒăꩂ%€ ‰€ ‚˙Running - Expansion: Isentropic (Ideal)I1@ŕ@0 0€2€°˜€ ƒƒăYQ߉€ ‚˙Isentropic (Real)e3—@EA2 4€f€€ ƒƒƒăŞ‚%€ ‰€ ‚˙Running - Expansion: Isentropic (Real)Bŕ@‡A0 0€$€°˜€ ƒƒăZQ߉€ ‚˙Isothermal^,EAĺA2 4€X€€ ƒƒƒă@Ş‚%€ ‰€ ‚˙Running - Expansion: Isothermalj.‡AOB< H€\€˜˜ă€‰€‚€ ƒă"&‰€ ‚˙Compressible FlowVelocity of SoundW&ĺAŚB1 2€L€€ ƒƒăŘg€ ‰€ ‚˙Running - Velocity of SoundAOBçB/ .€$€°˜€ ƒă#&‰€ ‚˙Mach NumberQ ŚB8C1 2€@€€ ƒƒăh€ ‰€ ‚˙Running - Mach Number@çBxC/ .€"€°˜€ ƒă$&‰€ ‚˙PropertiesB8CşC0 0€$€˜˜€ ƒƒă |‰€ ‚˙Stagnation]+xCD2 4€V€€ ƒƒƒăĽŐE.€ ‰€ ‚˙Running - Stagnation Properties>şCUD0 0€€°˜€ ƒƒă |‰€ ‚˙StaticY'DŽD2 4€N€€ ƒƒƒăĐŐE.€ ‰€ ‚˙Running - Static Properties< UDęD/ .€€°˜€ ƒă%&‰€ ‚˙NozzleJŽD4E3 6€.€˜˜€ƒƒăBƒ€ ‰€ ‚˙Nozzle (Ideal)U#ęD‰E2 4€F€€ƒƒƒă8 G.€ ‰€ ‚˙Running - Nozle (Ideal)I4EŇE3 6€,€˜˜€ƒƒăCƒ€ ‰€ ‚˙Nozzle (Real)U#‰E'F2 4€F€€ƒƒƒăc G.€ ‰€ ‚˙Running - Nozzle (Real)BŇEiF/ .€&€°˜€ ƒă&&‰€ ‚˙Normal ShockR!'FťF1 2€B€€ ƒƒă„h€ ‰€ ‚˙Running - Normal Shock>iFůF/ .€€°˜€ ƒă'&‰€ ‚˙DiffuserLťFEG3 6€2€˜˜€ƒƒă´‘€ ‰€ ‚˙Diffuser (Ideal)X&ůFG2 4€L€€ƒƒƒă^yI.€ ‰€ ‚˙Running - Diffuser (Ideal)KEGčG3 6€0€˜˜€ƒƒăľ‘€ ‰€ ‚˙Diffuser (Real)W%G?H2 4€J€€ƒƒƒă‰yI.€ ‰€ ‚˙Running - Diffuser (Real)< čG{H/ .€€°˜€ ƒă(&‰€ ‚˙ThrustJ?HĹH3 6€.€˜˜€ƒƒă혀 ‰€ ‚˙Thrust (Ideal)V${HI2 4€H€€ƒƒƒăńŻJ.€ ‰€ ‚˙Running - Thrust (Ideal)IĹHdI3 6€,€˜˜€ƒƒăľ‘€ ‰€ ‚˙Thrust (Real)U#IšI2 4€F€€ƒƒƒă°J.€ ‰€ ‚˙Running - Thrust (Real)1dIęI1m ˙˙˙˙˙˙˙˙˙˙˙˙ęI2„é°šIÓJ9 @€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+ęIţJ( €€˜˜‚Q€ ‚˙ŮÓJM< F€ł€€‚€‚€ €‚€ €‚‚‚‚‚‚‚˙Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power and Propulsion Systems Analysis, that quickly andreliably calculates thermodynamic and transport properties of gaseous,liquid and solid species, analyzes power cycles, power cyclecomponents/processes and compressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofŐţJ"O: B€Ť€€‚‚‚‚‚€ €€ €‚‚€ ‚˙energy conversion systems. It should provide you with the opportunityto more quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outmore about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (301) 540-3605.Thermodynamic and Transport PropertiesšMKd –€s€€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚˙Temperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressurePower CyclesCarnotBra"OKšIyton (Power and Propulsion)RankineOttoDieselPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowVelocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibilitye"Oځ* $€Ę€€ƒ‚ƒ‚ƒ‚ƒ‚˙80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:wIKQ‚. ,€’€†üEĄ€ƒƒ‚ƒƒ‚˙MicrosoftŽ Windows 98Ž, Windows 2000Ž,Windows MEŽ and Windows XPŽ ßځ\ƒ, &€ż€€‚‚‚‚‚ƒ‚‚‚˙Distributed on CD ROMFree Technical and Product Support30 Day Money Back GuaranteeTrademarks:All product names, company names andservice marks are trademarks or registered trademarks of theirrespective companies.ÖĽQ‚2„1 0€K€€‚€ ‚€‚‚‚‚‚‚˙Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1\ƒc„1s˙˙˙˙˙˙˙˙˙˙˙˙c„Ľ‹é°2„L…9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+c„w…( €€˜˜‚Q€ ‚˙ ËL…€‡> J€—€†ŘĄQ€‚€‚€ €‚‚‚‚‚‚‚‚‚‚˙Claim SheetEngineering Software products allow quick and reliablecalculation of thermodynamic and transport properties ofgaseous, liquid and solid species, contain coefficients forthe calculation of physical properties, steam approximationsfor both saturated and superheated areas, analyze powercycles, power cycle components/processes andcompressible flow.The aforementioned engineering calculations are valid underthe following assumptions:$âw…¤‰B R€Ĺ€†ŘĄQ€‚€ €‚‚‚‚‚‚‚‚‚‚€ ‚€‚˙Thermodynamic and Transport PropertiesSingle species considerationIdeal gas approach is used (pv=RT)Specific heat is not constantCoefficients describing thermodynamic and transport propertieswere obtained from the NASA Glenn Research Center at LewisField in Center in Cleveland, OH -- such coefficients conform withthe standard reference temperature of 298.15 K (77 F) and theJANAF tablesPower CyclesSingle species consideration -- fuel mass flow rate ignored andš€‡Ľ‹H ^€s€†ŘĄQ€‚‚‚‚‚€ €‚‚‚‚‚‚€ ‚€‚‚‚€‚˙its impact on the properties of the working fluidBasic equations hold (continuity, momentum and energyequations)Specific heat is constantPower Cycle Components/ProcessesSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constantCompressible FlowSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constant1¤‰Ö‹1N˙˙˙˙˙˙˙˙˙˙˙˙֋óŽé°Ľ‹żŒ9 @€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+֋ęŒ( €€˜˜‚Q€ ‚˙ ÎżŒóŽ; D€€†ŘĄQ€‚€‚€ ‚€‚‚‚‚‚‚˙How to Use the ProgramIn each section, subsection of the Power and Propulsion SystemsAnalysis program, the user needs to change one or more input values inorder to calculate a new case. Input values are in boxes with whitebackground and can be changed by clicking on each individual box oreven by using the arrow keys and changing the current value. Outputvalues cannot be modified, changed by the user and they are in boxeswith black background.1ęŒ$1Y˙˙˙˙˙˙˙˙˙˙˙˙$XĹé°óŽŔ9 @€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.enginee$ŔóŽring-4e.com+$DŔ( €€˜˜‚Q€ ‚˙7őŔ{ÂB R€ë€†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 thisCóDŔžÄP n€ç€†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, thenšm{ÂXĹ- *€Ú€†ŘĄQ€ €‚‚˙Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1žÄ‰Ĺ1˙˙˙˙˙˙˙˙˙˙˙˙‰ĹvÉé°XĹrĆ9 @€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+‰ĹĆ( €€˜˜‚Q€ ‚˙LrĆéĆ- *€>€†ŘĄQ€‚€‚˙Suggestion/Evaluation FormܝĆýÇ8 >€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‘]éƎČ4 8€ş€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:Q(ýÇßČ) "€P€ †ŘĄQ€ ‚˙Power and Propulsion Systems Analysis—ZŽČvÉ= J€´€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Quality:Usefulness:Possible areas of improvement:Other suggestions:1ßȧÉ1k˙˙˙˙˙˙˙˙˙˙˙˙§ÉáÎé°vɐĘ9 @€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+§ÉťĘ( €€˜˜‚Q€ ‚˙!ݐĘÜĚD V€ť€†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, andŃťĘáÎ4 6€Ł€†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 software1ÜĚĎ1ą˙˙˙˙˙˙˙˙˙˙˙˙ĎŁé°áÎ 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.comĎ áÎ+Ď7( €€˜˜‚Q€ ‚˙ß L6 :€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.7Ł) "€\€†ŘĄQ€‚˙steam table calculations are not available.1LÔ1˙˙˙˙˙˙˙˙˙˙˙˙Ô3é°Ł˝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+Ôč( €€˜˜‚Q€ ‚˙K˝39 @€%€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Temperature - PressureThis subsection provides physical properties of the selected species forassigned temperature and pressure.Input Values:Species, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1čd1Ľ˙˙˙˙˙˙˙˙ ˙˙˙˙dŘíą3Q< 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+d|( €€˜˜‚Q€ ‚˙"äQž> J€É€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Temperature - PressureSTEP 1Select the desired species or go with the default species.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:|Ř) "€"€†ŘĄQ€‚˙the Main menu.1ž 1‡˙˙˙˙˙˙˙˙ ˙˙˙˙ _ é°Řň 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€ ‚˙B ň _ 9 @€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Enthalpy - PressureThis subsection provides physical properties of the selected species forassigned enthalpy and pressure.Input Values:Species, Enthalpy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1  1—˙˙˙˙˙˙˙˙ ˙˙˙˙ öé°_ y 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€ ‚˙Űy ź= H€ˇ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Enthalpy - PressureSTEP 1Select the desired species or go with the default species.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:¤ ö) "€"€†ŘĄQ€‚˙the Main menu.1ź'1„˙˙˙˙˙˙˙˙ ˙˙˙˙'ƒAé°ö@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.engi'@öneering-4e.com+'G@( €€˜˜‚Q€ ‚˙<@ƒA8 >€ €†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Properties: Entropy - PressureThis subsection provides physical properties of the selected species forassigned entropy and pressure.Input Values:Species Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1G@´A1“˙˙˙˙˙˙˙˙ ˙˙˙˙´AE鰃AB9 @€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+´AČB( €€˜˜‚Q€ ‚˙םBÜD= H€Ż€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Properties: Entropy - PressureSTEP 1Select the desired species or go with the default speciesSTEP 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:ČBE) "€"€†ŘĄQ€‚˙the Main menu.1ÜDGE1 ˙˙˙˙˙˙˙˙˙˙˙˙GE#Gé°E0F9 @€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+GE[F( €€˜˜‚Q€ ‚˙Ș0F#G0 .€1€†ŘĄQ€‚€‚‚‚˙Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1[FTG1ç˙˙˙˙˙˙˙˙˙˙˙˙TG Ié°#G=H9 @€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+TGhH( €€˜˜‚Q€ ‚˙˘s=H I/ .€ć€†ŘĄQ€‚€‚‚‚˙Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto and Diesel).1hH;I1Ě˙˙˙˙˙˙˙˙˙˙˙˙;IÖKé° I$J9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+;IOJ( €€˜˜‚Q€ ‚˙‡N$JÖK9 @€€†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.1OJL1N˙˙˙˙˙˙˙˙˙˙˙˙L$Oé°ÖKđL9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+LM( €€˜˜‚Q€ ‚˙ ĚđL$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.1MUO1˙˙˙˙˙˙˙˙˙˙˙˙UO.é°$OJ€9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:infUOJ€$Oo@engineering-4e.comWeb Site:http://www.engineering-4e.com+UOu€( €€˜˜‚Q€ ‚˙š‰J€.0 .€€†ŘĄQ€‚€‚‚‚˙Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1u€_1˙˙˙˙˙˙˙˙˙˙˙˙_2…é°.H‚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+_s‚( €€˜˜‚Q€ ‚˙ŰH‚‰„; 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.Šs‚2…* $€ţ€†ŘĄQ€‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1‰„c…1i˙˙˙˙˙˙˙˙˙˙˙˙c…›Šé°2…L†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+c…w†( €€˜˜‚Q€ ‚˙@L†ˇˆ? 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 defaultäŤw†›Š9 @€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.1ˇˆ̊1\˙˙˙˙˙˙˙˙˙˙˙˙̊÷Ž鰛Šľ‹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+̊ŕ‹( €€˜˜‚Q€ ‚˙Űľ‹ô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 RateŐŕ‹÷Ž. *€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.1ô(1đ˙˙˙˙˙˙˙˙˙˙˙˙(ďĹé°÷ŽŔ9 @€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.eng(Ŕ÷Žineering-4e.com+(HŔ( €€˜˜‚Q€ ‚˙=ţŔ…Â? L€ý€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Power (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultAHŔĆÄ< 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)÷…ÂďĹ2 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.1ĆÄ Ć1˙˙˙˙˙˙˙˙˙˙˙˙ ĆĘé°ďĹ Ç9 @€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+ Ć4Ç( €€˜˜‚Q€ ‚˙9ý ÇmÉ< 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›q4ÇĘ* $€â€†ŘĄQ€‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1mÉ9Ę1m˙˙˙˙˙˙˙˙˙˙˙˙9ĘuĎé°Ę"Ë9 @€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+9ĘMË( €€˜˜‚Q€ ‚˙D"Ë‘Í? L€ €†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Propulsion (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3 Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultäŤMËuĎ9 @€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‘ÍŚĎ1Î˙˙˙˙˙˙˙˙˙˙˙˙ŚĎđé°uĎ›9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box ŚĎ›uĎ1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŚĎĆ( €€˜˜‚Q€ ‚˙I ›< 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.áśĆđ+ $€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!1ň˙˙˙˙˙˙˙˙˙˙˙˙!â íąđ< 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+!9( €€˜˜‚Q€ ‚˙B{? L€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultA9ź < 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{â 1 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.1ź  1Ú˙˙˙˙˙˙˙˙˙˙˙˙ ź é°â ü 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€ ‚˙•[ü ź : 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.1' í 1Â˙˙˙˙˙˙˙˙˙˙˙˙í ŞAé°ź Ö9 @€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+í ( €€˜˜‚Q€ ‚˙ÓÖA< 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 floAź w 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.ŽbŞA, (€Ä€†ŘĄQ€‚‚‚‚˙STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1AŰA1×˙˙˙˙˙˙˙˙˙˙˙˙ŰACé°ŞAÄB9 @€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+ŰAďB( €€˜˜‚Q€ ‚˙’dÄBC. ,€Č€†ŘĄQ€‚€‚‚˙Power Cycles: OttoThis subsection provides analysis of the Otto cycle for power applications.1ďB˛C1ę˙˙˙˙˙˙˙˙˙˙˙˙˛CkG鰁C›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+˛CĆD( €€˜˜‚Q€‚˙;›DG9 @€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: Otto: Power (Ideal)This subsection provides analysis of the Otto cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Revolutions, Fuel HHV,Number 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?ĆDkG+ &€~€†ŘĄQ€‚‚‚˙Assumptions:Specific heat is constant. Four stroke engine.1GœG1Ŕ˙˙˙˙˙˙˙˙˙˙˙˙œG+Né°kG…H9 @€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+œG°H( €€˜˜‚Q€ ‚˙4ő…HäJ? L€ë€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Otto: Power (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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°HM< 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&ôäJ+N2 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.1M\N1™˙˙˙˙˙˙˙˙ ˙˙˙˙\N}‚é°+NEO9 @€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+\NpO( €€˜˜‚Q€‚˙ÚEO9 @€ľ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: Otto: Power (Real)This subsection provides analysis of the Otto cycpO+Nle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Revolutions, Fuel HHV,Number of Cylinders, Cylinder Stroke, Stroke to Diameter Ratio,Compression Isentropic Efficiency, Combustor Efficiency, ExpansionIsentropic EfficiencyOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,îŔpO}‚. *€€†ŘĄQ€‚‚‚‚‚˙Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1Ž‚1c˙˙˙˙˙˙˙˙!˙˙˙˙Ž‚ŕŠé°}‚—ƒ9 @€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+Ž‚ƒ( €€˜˜‚Q€ ‚˙3ô—ƒő…? L€é€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Otto: Power (Real)STEP 1Select the desired working fluid or go with the default working fluid.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!ĺƒˆ< 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 Ôő…#Š9 @€Š€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙to diameter value.STEP 11Enter the desired compression isentropic efficiency value or go with thedefault compression isentropic efficiency value.STEP 12Enter the desired combustion efficiency value or go with thedefault combustion efficiency value.STEP 13Enter the desired expansion isentropic efficiency value or go with thedefault expansion isentropic efficiency value.STEP 14Click on the Calculate button to start the calculation of the Otto cycle˝ˆŕŠ. *€€†ŘĄQ€‚‚‚‚‚˙output values for the chosen input values.STEP 15When done with Steps 1 through 14, click on the Exit button to go backto the Main menu.1#Š‹1ŕ˙˙˙˙˙˙˙˙"˙˙˙˙‹ŔŒé°ŕŠú‹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+‹%Œ( €€˜˜‚Q€ ‚˙›mú‹ŔŒ. ,€Ú€†ŘĄQ€‚€‚‚˙Power Cycles: DieselThis subsection provides analysis of the Diesel cycle for both power applications.1%ŒńŒ1˙˙˙˙˙˙˙˙#˙˙˙˙ńŒËŔé°ŔŒڍ9 @€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+ńŒŽ( €€˜˜‚Q€ ‚˙B ڍSŔ9 @€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: Diesel: Power (Ideal)This subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Revolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfŽSŔŔŒficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelxLŽËŔ, (€˜€†ŘĄQ€‚‚‚‚˙ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1SŔüŔ1Ö˙˙˙˙˙˙˙˙$˙˙˙˙üŔĄÇé°ËŔĺÁ9 @€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+üŔÂ( €€˜˜‚Q€ ‚˙:űĺÁJÄ? L€÷€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Diesel: Power (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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,đÂvĆ< 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+ůJÄĄÇ2 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.1vĆŇÇ1[˙˙˙˙˙˙˙˙%˙˙˙˙ŇÇüËé°ĄÇťČ9 @€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+ŇÇćČ( €€˜˜‚Q€ ‚˙ŮťČ÷Ę8 >€ł€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: Diesel: Power (Real)This subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Revolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter Ratio, Compression Isentropic Efficiency,Combustion Efficiency, Expansion Isentropic EfficiencyOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,ÖćČüË/ ,€­€†ŘĄQ€‚‚‚‚‚‚˙Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelConsumptionAssumptions:Specific heat is constant. Four stroke engine.1÷Ę-Ě1ď ˙˙˙˙˙˙˙˙&˙˙˙˙-́é°üËÍ9 @€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+-ĚAÍ( €€˜˜‚Q€ ‚˙9úÍzĎ? L€ő€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycles: Diesel: Power (Real)STEP 1Select the desired working fluid or go with the default working fluid.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,đAͲ< F€á€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙cut-off ratio value.STEP 6Enter the desired number of revolutions valuzϲüËe 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 toŮzĎÄ9 @€ł€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙diameter ratio value.STEP 11Enter the desired compression isentropic efficiency value or go with thedefault compression isentropic efficiency value.STEP 12Enter the desired combustion efficiency value or go with thedefault combustion efficiency value.STEP 13Enter the desired expansion isentropic efficiency value or go with thedefault expansion isentropic efficiency value.STEP 14Click on the Calculate button to start the calculation of the Diesel cycle˝˛. *€€†ŘĄQ€‚‚‚‚‚˙output values for the chosen input values.STEP 15When done with Steps 1 through 14, click on the Exit button to go backto the Main menu.1IJ1˙˙˙˙˙˙˙˙'˙˙˙˙˛‡鰁›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+˛Ć( €€˜˜‚Q€ ‚˙Á‘›‡0 .€#€†ŘĄQ€‚€‚‚‚˙Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1Ƹ1Ř˙˙˙˙˙˙˙˙(˙˙˙˙¸_鰇Ą9 @€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€ ‚˙“eĄ_. ,€Ę€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1̐1ä˙˙˙˙˙˙˙˙)˙˙˙˙C é°_y 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€ ‚˙Ÿfy C 9 @€Í€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Compression: Isentropic (Ideal)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1¤ t 1ß˙˙˙˙˙˙˙˙*˙˙˙˙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€ ‚˙Ě] < F€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Compression: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.’]ˆ .@5 8€ť€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 5Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit but.@C ton to go back tothe Main menu.1_@1˙˙˙˙˙˙˙˙+˙˙˙˙_@4Cé°.@HA9 @€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€ ‚˙Á‡HA4C: B€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1sAeC1`˙˙˙˙˙˙˙˙,˙˙˙˙eC”Hé°4CND9 @€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+eCyD( €€˜˜‚Q€ ‚˙ ĚND‚F= H€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Compression: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.ŰyD”H7 <€ˇ€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙STEP 5Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Enter the desired compressor isentropic efficiency value or go with thedefault compressor isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1‚FĹH1Č˙˙˙˙˙˙˙˙-˙˙˙˙ĹH\K鰔HŽI9 @€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+ĹHŮI( €€˜˜‚Q€ ‚˙ƒJŽI\K9 @€•€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression1ŮIK1§˙˙˙˙˙˙˙˙.˙˙˙˙K€é°\KvL9 @€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+KĄL( €€˜˜‚Q€ ‚˙ ĚvLŤN> J€™€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Compression: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.STEP 5X%ĄL€3 4€K€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚˙Enter the desired compressor mass value or go with the defaultmass value.STEP 6Click on the Calculate button to start the calculation of compressor outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menuŤN€\K.1ŤN@€1Ö˙˙˙˙˙˙˙˙/˙˙˙˙@€ĺ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+@€T( €€˜˜‚Q€ ‚˙‘c)ĺ. ,€Ć€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1T‚1ş˙˙˙˙˙˙˙˙0˙˙˙˙‚Ÿ…é°ĺ˙‚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+‚*ƒ( €€˜˜‚Q€ ‚˙+đ˙‚U…; D€á€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Combustion: Coal/OilThis subsection provides analysis of the combustion process when coalor oil are considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!*ƒŸ…) "€B€†ŘĄQ€‚˙Specific heat is not constant.1U…Ѕ1ë˙˙˙˙˙˙˙˙1˙˙˙˙ЅŠŒ鰟…š†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+Ѕä†( €€˜˜‚Q€ ‚˙?š†#‰9 @€ €†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Combustion: Coal/OilSTEP 1Enter the desired fuel (coal or oil) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.áä†=‹9 @€Ă€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Furthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired stoichiometry (1 or > 1) or go with the default stoichiometry value.STEP 6Enter the desired combustion efficiency value or go with theM#‰ŠŒ1 0€9€†ŘĄQ€‚‚‚‚‚‚‚‚˙default combustion efficiency value.STEP 7Click on the Calculate button to start the calculation of combustion gascomposition and flame temperature value 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=‹ťŒ1˛˙˙˙˙˙˙˙˙2˙˙˙˙ťŒVŔ鰊Œ¤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+ťŒύ( €€˜˜‚Q€ ‚˙⤍ Ŕ; D€Ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Combustion: GasThis subsection provides analysis of the combustion process when gasis considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.ύ ŔŠŒJ!ύVŔ) "€B€†ŘĄQ€‚˙Specific heat is not constant.1 Ŕ‡Ŕ1ć˙˙˙˙˙˙˙˙3˙˙˙˙‡Ŕ<Çé°VŔpÁ9 @€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+‡Ŕ›Á( €€˜˜‚Q€ ‚˙2ůpÁÍĂ9 @€ó€†ŘĄQ€€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Combustion: GasSTEP 1Enter the desired fuel (gas) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you. ç›ÁíĹ9 @€Ď€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Furthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired stoichiometry value (1 or > 1) or go with the default stoichiometry value.STEP 6Enter the desired combustion efficiency value or go with theOÍĂ<Ç2 2€;€†ŘĄQ€‚‚‚‚‚‚‚‚‚˙default combustion efficiency value.STEP 7Click on the Calculate button to start the calculation of combustion gascomposition and flame temperature value for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1íĹmÇ1Ô˙˙˙˙˙˙˙˙4˙˙˙˙mÇÉé°<ÇVČ9 @€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+mǁČ( €€˜˜‚Q€ ‚˙aVČÉ. ,€Â€†ŘĄQ€‚€‚‚˙Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1ČAÉ1ß˙˙˙˙˙˙˙˙5˙˙˙˙AÉďËé°É*Ę9 @€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+AÉUĘ( €€˜˜‚Q€ ‚˙ša*ĘďË9 @€Ă€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Expansion: Isentropic (Ideal)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1UĘ Ě1Ł˙˙˙˙˙˙˙˙6˙˙˙˙ Ě÷é°ďË Í9 @€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+ Ě4Í( €€˜˜‚Q€ ‚˙Ü ÍLĎ< F€š€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Expansion: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine/expander inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine/expander inlet pressure value or go with thedefault pressure value.STEP 4Enter the desired turbine/expander outlet pressure value or go with thedefault pressure value.Ÿj4Í÷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 LĎ÷ďËthe 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.1LĎ(1ü˙˙˙˙˙˙˙˙7˙˙˙˙(óé°÷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€ ‚˙ˇ~ó9 @€ý€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processes: Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1<$1´˙˙˙˙˙˙˙˙8˙˙˙˙$§ é°ó 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+$8( €€˜˜‚Q€ ‚˙Ű O< F€ˇ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Expansion: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine/expander inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine/expander inlet pressure value or go with thedefault pressure value.STEP 4Enter the desired turbine/expander outlet pressure value or go with thedefault pressure value. č8o 8 >€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 to8O§ ( € €†ŘĄQ€˙the Main menu.1o Ř 1Á˙˙˙˙˙˙˙˙9˙˙˙˙Ř h é°§ Á 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+Ř ě ( €€˜˜‚Q€ ‚˙|CÁ h 9 @€‡€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycle Components/Processs: Expansion: IsothermalThis subsection provides analysis of isothermal expansion.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal expansion1ě ™ 1P˙˙˙˙˙˙˙˙:˙˙˙˙™ !Aé°h ‚ 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€ ‚˙<ý‚  @? L€ű€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power Cycle Components/Processes: Expansion: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired turbine inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired turbine mass value or go with the default­  @h ă­ !A2 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.1 @RA1ž˙˙˙˙˙˙˙˙;˙˙˙˙RAßBé°!A;B9 @€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+RAfB( €€˜˜‚Q€ ‚˙yK;BßB. ,€–€†ŘĄQ€‚€‚‚˙Compressible FlowThis section provides analysis of compressible flow.1fBC1S˙˙˙˙˙˙˙˙<˙˙˙˙C2Eé°ßBůC9 @€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€ ‚˙ÖůC2E8 >€­€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Velocity of SoundThis subsection provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1$DcE12˙˙˙˙˙˙˙˙=˙˙˙˙cEdHé°2ELF9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+cEwF( €€˜˜‚Q€ ‚˙íąLFdH< F€c€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Velocity of SoundSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Click on the Calculate button to start the calculation of velocity of soundvalue for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1wF•H1K˙˙˙˙˙˙˙˙>˙˙˙˙•HŻJé°dH~I9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+•HŠI( €€˜˜‚Q€ ‚˙Î~IŻJ8 >€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1ŠIŕJ1Ł˙˙˙˙˙˙˙˙?˙˙˙˙ŕJRNé°ŻJÉK9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŕJôK( €€˜˜‚Q€ ‚˙$ćÉKN> J€Í€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Mach NumberSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Enter the desired velocity value or go with the default velocity value.STEP 4Click on 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:ôKRN) "€"€†ŘĄQ€‚˙the Main menu.1NƒN1˙˙˙˙˙˙˙˙@˙˙˙˙ƒNb€íąRNpO< 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+ƒN›O( €€˜˜‚Q€ ‚˙ť‹pOb€0 .€€†ŘĄQ€‚€‚‚‚˙Compressible Flow: PropertiesThis subsection pro›Ob€RNvides analysis of stagnation and static properties inthe case of compressible flow.1›O“€1ˆ˙˙˙˙˙˙˙˙A˙˙˙˙“€ę‚é°b€|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€ ‚˙C |ę‚8 >€€†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 constant1§ƒ1D˙˙˙˙˙˙˙˙B˙˙˙˙ƒ.‡é°ę‚„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+ƒ/„( €€˜˜‚Q€ ‚˙'é„V†> J€Ó€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Properties: StagnationSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired static temperature value or go with the default statictemperature value.STEP 3Enter the desired static pressure value or go with the default staticpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of stagnationŘŞ/„.‡. *€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.1V†_‡1|˙˙˙˙˙˙˙˙C˙˙˙˙_‡މé°.‡Hˆ9 @€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+_‡sˆ( €€˜˜‚Q€ ‚˙7˙Hˆމ8 >€˙€†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 constant1sˆۉ1L˙˙˙˙˙˙˙˙D˙˙˙˙ۉöíąŞ‰Ȋ< 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+ۉóŠ( €€˜˜‚Q€ ‚˙/ńȊ"> J€ă€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Properties: StaticSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of staticÔŚóŠö. *€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"'Ž1Ă˙˙˙˙˙˙˙˙E˙˙˙˙'Žšíąö< 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+'Ž?( €€˜˜‚Q€ ‚˙zLš. ,€˜€†ŘĄQ€‚€‚‚˙Compressible Flow: NozzleThis subsection provides analysis of nozzle.1? Ŕ1"˙˙˙˙˙˙˙˙F˙˙˙˙ Ŕmš ŔšíąšůŔ< 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+ Ŕ$Á( €€˜˜‚Q€ ‚˙IůŔmÂ8 >€#€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Nozzle (Ideal)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1$ÁžÂ1Y˙˙˙˙˙˙˙˙G˙˙˙˙žÂĆĆé°m‡Ă9 @€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+žÂ˛Ă( €€˜˜‚Q€ ‚˙0ň‡ĂâĹ> J€ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Nozzle (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of Mach number,侲ĂĆĆ/ ,€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.1âĹ÷Ć1ă˙˙˙˙˙˙˙˙H˙˙˙˙÷ĆŠÉíąĆĆäÇ< 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+÷ĆČ( €€˜˜‚Q€ ‚˙š`äÇŠÉ: B€Á€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Nozzle (Real)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, Ideal Velocity,Nozzle EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, StaticTemperature, Velocity, Mach NumberAssumptions:Specific heat is constant1ČÚÉ1ž˙˙˙˙˙˙˙˙I˙˙˙˙ÚÉgÎé°ŠÉĂĘ9 @€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+ÚÉîĘ( €€˜˜‚Q€ ‚˙0ňĂĘÍ> J€ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Nozzle (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired nozzle efficiency value or go with the default nozzleIîĘgÎ3 4€-€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚˙efficiency value.STEP 6Click on the Calculate button to start the calculation of Mach number,stagnation temperature and stagnation pressure values for the choseninput values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1͘Î1˘˙˙˙˙˙˙˙˙J˙˙˙˙˜Îżé°g΁Ď9 @€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+˜ÎŹĎ( €€˜˜‚Q€ ‚˙ˁϿ< F€—€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: NorŹĎżgÎmal ShockThis subsection provides analysis of normal shock.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet StagnationPressure, Inlet VelocityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach NumberOutlet Stagnation Temperature, Outlet Stagnation Pressure, OutletVelocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1ŹĎđ1Ú˙˙˙˙˙˙˙˙K˙˙˙˙đ™é°żŮ9 @€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€ ‚˙K ŮO? L€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Normal ShockSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired inlet stagnation temperature value or go with thedefault inlet stagnation temperature value.STEP 3Enter the desired inlet stagnation pressure value or go with the defaultinlet stagnation pressure value.STEP 4Enter the desired inlet velocity value or go with the default velocityvalue.STEP 5Click on the Calculate button to start the calculation of inlet MachJ™0 .€5€†ŘĄQ€‚‚‚‚‚‚‚˙number, 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.1OĘ1Ç˙˙˙˙˙˙˙˙L˙˙˙˙Ę`íą™ˇ< 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+Ęâ( €€˜˜‚Q€ ‚˙~Pˇ`. ,€ €†ŘĄQ€‚€‚‚˙Compressible Flow: DiffuserThis subsection provides analysis of diffuser.1â‘1’˙˙˙˙˙˙˙˙M˙˙˙˙‘ň é°`z 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+‘Ľ ( €€˜˜‚Q€ ‚˙Mz ň 8 >€+€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Diffuser (Ideal)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1Ľ # 1K˙˙˙˙˙˙˙˙N˙˙˙˙# =é°ň  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+# 7 ( €€˜˜‚Q€ ‚˙"ä Y> J€É€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Diffuser (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired static temperature value or go with the default statictemperature value.STEP 3Enter the desired static pressure value or go with the default staticpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of Mach number,äľ7 =/ ,€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.1Yn1×˙˙˙˙˙˙˙˙O˙˙˙˙nBé°=c@9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (nc@=301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+nŽ@( €€˜˜‚Q€ ‚˙Gc@B: B€€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Diffuser (Real)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, Velocity,Diffuser EfficiencyOutput Values:Mach Number, Ideal Stagnation Temperature, Stagnation Pressure,Stagnation TemperatureAssumptions:Specific heat is constant1Ž@@B1´˙˙˙˙˙˙˙˙P˙˙˙˙@BĂFé°B)C9 @€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+@BTC( €€˜˜‚Q€ ‚˙&č)CzE> J€Ń€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Diffuser (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired static temperature value or go with the default statictemperature value.STEP 3Enter the desired static pressure value or go with the default staticpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired diffuser efficiency value or go with the default diffuserITCĂF3 4€-€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚˙efficiency value.STEP 6Click on the Calculate button to start the calculation of Mach number,stagnation temperature and stagnation pressure values for the choseninput values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1zEôF1Ă˙˙˙˙˙˙˙˙Q˙˙˙˙ôF†HíąĂFáG< 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+ôF H( €€˜˜‚Q€ ‚˙zLáG†H. ,€˜€†ŘĄQ€‚€‚‚˙Compressible Flow: ThrustThis subsection provides analysis of thrust.1 HˇH1Ç˙˙˙˙˙˙˙˙R˙˙˙˙ˇHMK鰆H I9 @€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+ˇHËI( €€˜˜‚Q€ ‚˙‚I IMK9 @€“€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Thrust (Ideal)This subsection provides analysis of thrust.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Stagnation Temperature,Stagnation Pressure, Velocity, Ambient PressureOutput Values:Static Temperature, Static Pressure, Mach Number, ThrustAssumptions:Specific heat is constant1ËI~K1A˙˙˙˙˙˙˙˙S˙˙˙˙~Kv€é°MKgL9 @€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€ ‚˙1ógLĂN> J€ç€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Thrust (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired mass flow rate value or go with the default mass flow§p’Lv€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 choseninputĂNv€MK values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1ĂN§€1˙˙˙˙˙˙˙˙T˙˙˙˙§€ƒé°v€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+§€ť( €€˜˜‚Q€ ‚˙Ň˜ƒ: B€1€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Thrust (Real)This subsection provides analysis of thrust.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Stagnation Temperature,Stagnation Pressure, Ideal Velocity, Ambient Pressure, Thrust EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, Thrust,Static Temperature, Velocity, Mach NumberAssumptions:Specific heat is constant1ťžƒ1‚˙˙˙˙˙˙˙˙U˙˙˙˙žƒ‰鰍ƒ§„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+žƒ҄( €€˜˜‚Q€ ‚˙0ň§„‡> J€ĺ€†ŘĄQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow: Thrust (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired stagnation temperature value or go with the defaultstagnation temperature value.STEP 3Enter the desired stagnation pressure value or go with the defaultstagnation pressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired mass flow rate value or go with the default mass flow Ň҄‰; D€Ľ€†ŘĄQ€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙rate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Enter the desired thrust efficiency value or go with the default thrustefficiency value.STEP 8Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1‡˙˙˙˙1˙˙˙˙˙˙˙˙V˙˙˙˙˙˙˙˙˙˙˙˙Ą4˜4˜č3Helv^ &‰G"˙Fë Ä^ &Tms Rmn&‹GZ™RP&‹GXÄSymbolPš\<ĄŽÄ^ &‰G"Courier^ ‹F‹V$Times New Roman5Ä^Arial&‹Ńč-@Ä^ &‰GMS SerifŠĐč*ä-@Ä^MS Sans SerifÇG'+TimesÄ^&öt#&‹HelveticaáŃáى^đŒFSystemë"&ŠĐč*ä‹Courier New‰^đŒFň&‰Roman^đ&öG*@t/Ä^&öScriptŃčÄ^đ&‰G+ƒFModern*äÄ^đ&‰G+˙FëMarlettÄ^&‹GZ™RP&‹Arial CEg*ż&‹G)÷éRPArial CYRG)FŽF &9u'Arial Greek-Ľ‹F+FřArial TURěƒěWVĹv ‹Arial BalticŽ@˙š´ŻCourier New CEö€~ěCourier New CYRöWš˛Courier New GreekŤ¸Courier New TURWV+ŔCourier New BalticuLucida Console‹Fú‹Lucida Sans UnicodeTimes New Roman CETimes New Roman CYRTimes New Roman GreTimes New Roman TURTimes New Roman BalWingdingséť&ƒ}˙uVerdanaŕ‰FâĆFć‹N‹Arial Black‹G‰FäëComic Sans MSPšükŤGeorgiaFŕPššeúłŽFţFranklin Gothic MedPalatino Linotype˙wTahoma&ěłÄ^Ô&˙w&˙wTrebuchet MS´šˆeW˛WebdingsÔ ‹Ć‹VúëEstrangelo 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