?_€’’’’—pgl …UGulimChe Tur?UGulimChe Baltic@U@GulimChe CEAU@Gul-#Cyrē [+ļJ[+’’Ö~ĒBr’’’’śpĒB@G-#e Tu÷ [+ ’’ĘxC:\WINDOWS\TEMP\~hc9 nowidctlparcs16super#Engineering Softwaree%’’’’’’’’Q’’’’’’’’’’’’# [+N-#ĒBż[+P[+’’ōxĒBŒ’’’’Y,xĒB E-#ĒB[+P[+’’š|ĒBŒ’’’’ĘxĒB†Ų-#[+P[+’’Œą;Łž*Ę2·JĒBją.j:#ĒB’’"BĒBśOńO’’’’ 1’’’’=1ŗ’’’’’’’’=Šé° &9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.comd>=Š& €|€°°€‚’Physical Properties and SteamApproximations 1.1 - Tutorial&¤} Ȁ;€°˜ć\ŖÓP€‰€‚ćS?€‰€‚ć$ēdI€‰€‚ćĢ’§n€‰€‚ć\–€‰€‚ćf¢v“€‰€‚怉€‚’Program DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPropertiesPŠō2 4€<€˜˜€ƒć> € ‰€ ‚’Temperature - Pressure\+¤P1 2€V€€ƒƒćŒ€ ‰€ ‚’Running - Temperature - PressureMō2 4€6€°˜€ƒć? € ‰€ ‚’Enthalpy - PressureY(Pö1 2€P€€ ƒƒć·€ ‰€ ‚’Running - Enthalpy - PressureLB2 4€4€°˜€ƒć@ € ‰€ ‚’Entropy - PressureX'öš1 2€N€€ƒƒćā€ ‰€ ‚’Running - Entropy - PressureFBą2 4€(€°˜€ƒćA € ‰€ ‚’CoefficientsR!š21 2€B€€ƒƒć Ž€ ‰€ ‚’Running - CoefficientsHąz. ,€4€°˜ć€‰€‚’Steam ApproximationsH2Ā2 4€,€˜˜€ƒćw€ ‰€ ‚’Saturated Area±qzs@ P€ā€€ƒƒćNåł€ ‰€ ‚€ ƒƒćyåł‰€ ‚’Running - Saturated Area - Temperature DependentRunning - Saturated Area - Pressure DependentJ½2 4€0€°˜€ƒćx€ ‰€ ‚’Superheated AreaV%s1 2€J€€ƒƒćJÄ€ ‰€ ‚’Running - Superheated Area1½D1$ ’’’’’’’’’’’’DC@ė±/: B€c€†Ų”Q€€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+DZ( €€˜˜‚Q€ ‚’-ń/‡ < F€ć€€‚€‚€ €‚€ €‚‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Physical Properties and Steam Approximations, thatquickly and reliably calculates thermodynamic and transport propertiesof gaseous, liquid and solid species and steam approximations.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunity×ZŸ A P€Æ€€‚‚‚‚‚€ €€ €‚‚€ ‚€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 PressureO‡ ī A P€€€ƒ‚‚€ ‚€ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚’Entropy and PressureSteam ApproximationsSaturated Area (Temperature and Pressure Dependent)Superheated AreaHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:h:Ÿ V. ,€t€†üE”€ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ßī a, &€æ€€‚‚‚‚‚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.Ö„VC@1 0€K€€‚€ ‚€‚‚‚‚‚‚’Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: aC@info@engineering-4e.comhttp://www.engineering-4e.com1at@1q’’’’’’’’’’’’t@“Gė±C@_A: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+t@ŠA( €€˜˜‚Q€ ‚’ Ė_A“C> J€—€†Ų”Q€‚€‚€ €‚‚‚‚‚‚‚‚‚‚’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:"ąŠAµEB R€Į€†Ų”Q€‚€ €‚‚‚‚‚‚‚‚‚‚€ ‚€‚’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’·“C“GH ^€o€†Ų”Q€‚‚‚‚‚€ €‚‚‚‚‚‚€ ‚€‚‚‚€‚’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 constant1µEåG1W’’’’’’’’’’’’åG K뱓GŠH: B€c€†Ų”Q€€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+åGūH( €€˜˜‚Q€ ‚’ÕŠH K; D€«€†Ų”Q€‚€‚€ ‚€‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Physical Properties and SteamApproximations program, the user needs to change one or moreinput values in order to calculate a new case. Input values are inboxes with white background and can be changed by clicking oneach individual box or even by using the arrow keys and changingthe current value. Output values cannot be modified, changed bythe user and they are in boxes with black background.1ūH€†Ų”Q€‚€‚’Suggestion/Evaluation Formܵ‚„8 >€¹€ †Ų”Q€‚‚€ ‚€‚‚‚‚‚‚’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‘]ƒ¦„4 8€ŗ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:X/„ž„) "€^€ †Ų”Q€ ‚’Physical Properties and Steam Approximations—Z¦„•…= J€“€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Quality:Usefulness:Possible areas of improvement:Other suggestions:1ž„Ę…1j’’’’’’’’’’’’ʅ’Šė±•…±†: B€c€†Ų”Q€€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+ʅ܆( €€˜˜‚Q€ ‚’ ܱ†üˆD V€¹€†Ų”Q€‚€‚€ €‚€ €‚‚‚‚‚‚‚‚‚’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 andĻ܆’Š4 6€Ÿ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚’- 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 software1üˆ0‹1³’’’’’’’’’’’’0‹²Žė±’ŠŒ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+0‹FŒ( €€˜˜‚Q€ ‚’ߌ[Ž6 :€æ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚’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.FŒ²Ž) "€\€†Ų”Q€‚’steam table calculations are not available.1[ŽćŽ1’’’’’’’’’’’’ćŽUĮė±²ŽĪ: B€c€†Ų”Q€€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+ćŽ Ą( €€˜˜‚Q€ ‚’Ī Ą²ŽIĪUĮ9 @€!€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’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 constant1 Ą†Į1„’’’’’’’’ ’’’’†ĮśÄļ²UĮuĀ= H€e€†Ų”Q€€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+†Į Ā( €€˜˜‚Q€ ‚’ āuĀĄÄ> J€Å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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: ĀśÄ) "€"€†Ų”Q€‚’the Main menu.1ĄÄ+Å1‡’’’’’’’’ ’’’’+ŁĒė±śÄĘ: B€c€†Ų”Q€€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++ÅAĘ( €€˜˜‚Q€ ‚’@ʁĒ9 @€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’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 constant1AƲĒ1—’’’’’’’’ ’’’’²ĒĖė±ĒČ: B€c€†Ų”Q€€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+²ĒČČ( €€˜˜‚Q€ ‚’ŁČŽŹ= H€³€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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:ČČĖ) "€"€†Ų”Q€‚’the Main menu.1ŽŹIĖ1‚’’’’’’’’ ’’’’I˚Ķė±Ė4Ģ: B€c€†Ų”Q€€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+IĖ_Ģ( €€˜˜‚Q€ ‚’;4̚Ķ8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’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 constant1_ĢĖĶ1Q’’’’’’’’ ’’’’ĖĶ:뱚ͶĪ: B€c€†Ų”Q€€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+ĖĶįĪ( €€˜˜‚Q€ ‚’Ö¶Ī= H€­€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 vaįĪšĶlue 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:įĪ:) "€"€†Ų”Q€‚’the Main menu.1k1’’’’’’’’’’’’kIė±:V: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+k( €€˜˜‚Q€ ‚’(ķV©; D€Ū€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 vI* $€ģ€†Ų”Q€‚‚’temperature intervals, 273 to 1,000 K and 1,000 to 5,000 K. The data havebeen constrained to be equal at 1,000 K.1©z1«’’’’’’’’’’’’zōė±Ie: B€c€†Ų”Q€€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+z( €€˜˜‚Q€ ‚’d,eō8 >€Y€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Running: CoefficientsSTEP 1Select the desired specie or go with the default specie.STEP 2Read and/or print the coefficients for the calculation of the physicalproperties for the chosen specie.STEP 3When done with Steps 1 through 2, click on the Exit button to go back tothe Main menu.1%1’’’’’’’’’’’’% ė±ō : B€c€†Ų”Q€€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€ ‚’Ș  0 .€1€†Ų”Q€‚€‚‚‚’Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1; 4 1’’’’’’’’’’’’4  ė±  : B€c€†Ų”Q€€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 J ( €€˜˜‚Q€ ‚’»ƒ  8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’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 Properties1J 6 1Ø’’’’’’’’’’’’6 ›@ė± !: B€c€†Ų”Q€€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 L( €€˜˜‚Q€ ‚’ Ģ!a@= H€™€†Ų”Q€‚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 valueLa@ s.STEP 4When done with Steps 1 through 3, click on the Exit button to go back to:L›@) "€"€†Ų”Q€‚’the Main menu.1a@Ģ@1W’’’’’’’’’’’’Ģ@ņCė±›@·A: B€c€†Ų”Q€€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+Ģ@āA( €€˜˜‚Q€ ‚’Ņ·AņC> J€„€†Ų”Q€‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Steam Approximations:Saturated Area: Pressure DependentSTEP 1Enter the desired saturated steam pressure value or go with the defaultpressure value.STEP 2Enter the desired steam quality or go with the default steam quality value.STEP 3Click on the Calculate button to start the calculation of the steamproperties for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1āA#D1©’’’’’’’’’’’’#D›Fė±ņCE: B€c€†Ų”Q€€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+#D9E( €€˜˜‚Q€ ‚’b,E›F6 :€Y€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚’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 Properties19EĢF1Y’’’’’’’’’’’’ĢFōIė±›F·G: B€c€†Ų”Q€€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+ĢFāG( €€˜˜‚Q€ ‚’Õ·GōI= H€«€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.1āG%J1 ’’’’’’’’’’’’%J’Kė±ōIK: B€c€†Ų”Q€€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€ ‚’ĔK’K0 .€)€†Ų”Q€‚€‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1;K0L1Ī’’’’’’’’’’’’0LĶNė±’KM: B€c€†Ų”Q€€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+0LFM( €€˜˜‚Q€ ‚’‡NMĶN9 @€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’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.1FMžN1R’’’’’’’’’’’’žN@‚ė±ĶN €: B€c€†Ų”Q€€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.comžN €ĶN+žN7€( €€˜˜‚Q€ ‚’ Ģ €@‚= H€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.17€q‚1’’’’’’’’’’’’q‚@„ė±@‚\ƒ: B€c€†Ų”Q€€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‚‡ƒ( €€˜˜‚Q€ ‚’¹‰\ƒ@„0 .€€†Ų”Q€‚€‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1‡ƒq„1’’’’’’’’’’’’q„Fˆė±@„\…: B€c€†Ų”Q€€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„‡…( €€˜˜‚Q€ ‚’Ū\…‡; D€·€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.©‡…Fˆ* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1‡wˆ1k’’’’’’’’’’’’wˆ±ė±Fˆb‰: B€c€†Ų”Q€€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+wˆ‰( €€˜˜‚Q€ ‚’@b‰Ķ‹? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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䫍‰±9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.1Ķ‹ā1Ė’’’’’’’’’’’’āĀĮė±±ĶŽ: B€c€†Ų”Q€€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+āųŽ( €€˜˜‚Q€ ‚’ŚĶŽĮ; D€µ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 ųŽĮ±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.©ųŽĀĮ* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1ĮóĮ1j’’’’’’’’’’’’óĮ,Ēė±ĀĮŽĀ: B€c€†Ų”Q€€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+óĮ Ć( €€˜˜‚Q€ ‚’?ŽĀHÅ? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 defaultä« Ć,Ē9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.1HÅ]Ē1’’’’’’’’’’’’]ĒGĖė±,ĒHČ: B€c€†Ų”Q€€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+]ĒsČ( €€˜˜‚Q€ ‚’9żHȬŹ< F€ū€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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›qsČGĖ* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1¬ŹxĖ1ą’’’’’’’’’’’’xĖĆė±GĖcĢ: B€c€†Ų”Q€€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+xĖŽĢ( €€˜˜‚Q€ ‚’EcĢÓĪ? L€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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䫎ĢĆ9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 ÓĪĆGĖstart 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.1ÓĪō1’’’’’’’’ ’’’’ōŻė±Ćß: B€c€†Ų”Q€€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+ō ( €€˜˜‚Q€ ‚’8üßB< F€ł€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Propulsion (Real)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine power›q Ż* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1B1o’’’’’’’’!’’’’L ė±Żł: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+$( €€˜˜‚Q€ ‚’Dłh? L€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultä«$L 9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1h} 1Ü’’’’’’’’"’’’’} ( ė±L h : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+} “ ( €€˜˜‚Q€ ‚’•[h ( : B€·€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: RankineThis subsection provides analysis of the Rankine cycle.Input Values:Turbine Inlet Conditions (Temperature and Pressure), Steam Mass FlowRate, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion and heattransfer.1“ Y 1’’’’’’’’#’’’’Y Aė±( D: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Y o( €€˜˜‚Q€ ‚’ÓDŠ@< F€§€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: RankineSTEP 1Select the desired steam turbine inlet conditions (temperature andpressure values) or go with the default selection.STEP 2Enter the steam mass flow rate value or go with the default steam massflow rate value.STEP 3Enter the desired fuel HHV value or go with the default fuel HHV value.SoŠ@( TEP 4Click on the Calculate button to start the calculation of the Rankine cycleoutput values for the chosen input values.ŽboA, (€Ä€†Ų”Q€‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1Š@IA1Ū’’’’’’’’$’’’’IAóDė±A4B: B€c€†Ų”Q€€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+IA_B( €€˜˜‚Q€‚’*ń4B‰D9 @€ć€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: OttoThis subsection provides analysis of the Otto cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Combustion Temperature, Number of Resolutions, Fuel HHVNumber of Cylinders, Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel Consumptionj?_BóD+ &€~€†Ų”Q€‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1‰D$E1·’’’’’’’’%’’’’$EŖKė±óDF: B€c€†Ų”Q€€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€ ‚’)źFcH? L€Õ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: OttoSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired combustion temperature value or go with the default!å:F„J< F€Ė€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’temperature value.STEP 6Enter the desired number of resolutions value or go with the defaultnumber of resolutions 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&ōcHŖK2 2€é€†Ų”Q€‚‚‚‚‚‚‚‚‚’to diameter value.STEP 11Click on the Calculate button to start the calculation of the Otto cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1„JŪK1ń’’’’’’’’&’’’’ŪK›Oė±ŖKĘL: B€c€†Ų”Q€€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+ŪKńL( €€˜˜‚Q€ ‚’2łĘL#O9 @€ó€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: DieselThis subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Resolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelxLńL›O, (€˜€†Ų”Q€‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1#OĢO1T’’’’’’’’'’’’’ĢOt†ė±›Oƀ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒĢOƀ›O‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĢOī€( €€˜˜‚Q€ ‚’/šƀƒ? L€į€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: DieselSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired cut-off ratio (volumetric) value or go with the default,šī€I…< F€į€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’cut-off ratio value.STEP 6Enter the desired number of resolutions value or go with the defaultnumber of resolutions 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+łƒt†2 2€ó€†Ų”Q€‚‚‚‚‚‚‚‚‚’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.1I…„†1•’’’’’’’’(’’’’„† ‹ė±t†‡: B€c€†Ų”Q€€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€ ‚’2ł‡ķ‰9 @€ó€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: MagnetohydrodynamicsThis subsection provides analysis of the Magnetohydrodynamics cycle.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet Stagnation Pressure,Velocity, Conductivity, Loading Parameter, Magnetic Field Strength,Channel Length, MobilityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Hall Voltage, Outlet StaticTemperature, Outlet Static Pressure, Outlet Mach Number, Outletķ»‡ ‹/ ,€Ū€†Ų”Q€‚‚‚‚‚‚’Stagnation Temperature, Outlet Stagnation Pressure, Specific WorkOutput, Enthalpy ExtractionAssumptions:Specific heat, velocity, conductivity, mobility, induced voltage field, Hallvoltage and magnetic field strength are constant.1ķ‰:‹1ļ’’’’’’’’)’’’’:‹hĮė± ‹%Œ: B€c€†Ų”Q€€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+:‹PŒ( €€˜˜‚Q€ ‚’4ö%Œ„Ž> J€ķ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 PŒŲĄ< F€€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 d„ŽŲĄ ‹esired 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„ŽhĮ, (€Č€†Ų”Q€‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1ŲĄ™Į1Ā’’’’’’’’*’’’’™Į*Äė±hĮ„Ā: B€c€†Ų”Q€€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+™ĮÆĀ( €€˜˜‚Q€ ‚’߄½Ć/ ,€æ€€‚€‚‚‚‚‚‚‚‚’Power Cycles: Fuel CellThis subsection provides analysis of the Fuel Cell cycle.Input Values:Fuel, Fuel Inlet Temperature, Oxidant (O2) Inlet Temperature,Fuel Flow Rate, Product Outlet TemperatureOutput Values:mDÆĀ*Ä) "€ˆ€†Ų”Q€‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1½Ć[Ä1’’’’’’’’+’’’’[ĹČė±*ÄFÅ: B€c€†Ų”Q€€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+[ÄqÅ( €€˜˜‚Q€ ‚’ įFÅ‘Ē? L€Ć€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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(öqŹČ2 2€ķ€†Ų”Q€‚‚‚‚‚‚‚‚‚’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.1‘ĒźČ1’’’’’’’’,’’’’źČŲŹė±¹ČÕÉ: B€c€†Ų”Q€€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+źČŹ( €€˜˜‚Q€ ‚’ŲØÕÉŲŹ0 .€Q€†Ų”Q€‚€‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1Ź Ė1Ś’’’’’’’’-’’’’ ˲Ģė±ŲŹōĖ: B€c€†Ų”Q€€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+ ĖĢ( €€˜˜‚Q€ ‚’“eō˲Ģ. ,€Ź€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1ĢćĢ1ō’’’’’’’’.’’’’ć̦Ļė±²ĢĪĶ: B€c€†Ų”Q€€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+ćĢłĶ( €€˜˜‚Q€ ‚’­pĪͦĻ= H€į€†Ų”Q€‚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.1łĶ×Ļ1j’’’’’’’’/’’’’×ĻŠ뱦ĻĪ: B€c€†Ų”Q€€×ĻĪ¦Ļƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+×Ļł( €€˜˜‚Q€ ‚’ ĒĪB R€€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Compression: Isentropic (Ideal)STEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.STEP 5ˆUłŠ3 4€«€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’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»1ó’’’’’’’’0’’’’»}뱊¦: B€c€†Ų”Q€€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+»Ń( €€˜˜‚Q€ ‚’¬o¦}= H€ß€†Ų”Q€‚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.1Ń®1×’’’’’’’’1’’’’®T ė±}™: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+®Ä( €€˜˜‚Q€ ‚’Ę™Ģ B R€€†Ų”Q€‚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 5ˆUÄT 3 4€«€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’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.1Ģ … 1×’’’’’’’’2’’’’… +ė±T p : B€c€†Ų”Q€€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€ ‚’Sp += H€§€†Ų”Q€‚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› \1·’’’’’’’’3’’’’\×Cė±+S@: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-\S@+Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+\~@( €€˜˜‚Q€ ‚’AžS@æBC T€ż€†Ų”Q€‚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 defaultę~@×C2 2€Ķ€†Ų”Q€‚‚‚‚‚‚‚‚‚’mass value.STEP 6Click on the Calculate button to start the calculation of compressor outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1æBD1Ų’’’’’’’’4’’’’DÆEė±×CóD: B€c€†Ų”Q€€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+DE( €€˜˜‚Q€ ‚’‘cóDÆE. ,€Ę€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1EąE1©’’’’’’’’5’’’’ąEXI뱯EĖF: B€c€†Ų”Q€€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+ąEöF( €€˜˜‚Q€ ‚’ŁĖFI? L€³€†Ų”Q€‚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!öFXI) "€B€†Ų”Q€‚’Specific heat is not constant.1I‰I1’’’’’’’’6’’’’‰I €ė±XItJ: B€c€†Ų”Q€€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+‰IŸJ( €€˜˜‚Q€ ‚’BtJįL< F€ €†Ų”Q€‚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.%ėŸJO: B€×€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 gasÓ¦įL €- (€M€†Ų”Q€‚‚‚‚’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.O €XI1O=€1°’’’’’’’’7’’’’=€؃ė± €(: B€c€†Ų”Q€€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+=€S( €€˜˜‚Q€ ‚’ Ģ(^ƒ? L€™€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Combustion: GasThis subsection provides analysis of the combustion process when gasis considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Oxidant to Fuel RatioOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Stoichiometry, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!S؃) "€B€†Ų”Q€‚’Specific heat is not constant.1^ƒك1x’’’’’’’’8’’’’ك Š뱨ƒĄ: B€c€†Ų”Q€€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+كļ„( €€˜˜‚Q€ ‚’7śĄ&‡= H€õ€†Ų”Q€‚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.%ėļ„K‰: B€×€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 gasÕ§&‡ Š. *€O€†Ų”Q€‚‚‚‚‚’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.1K‰QŠ1Ö’’’’’’’’9’’’’QŠö‹ė± Š<‹: B€c€†Ų”Q€€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+QŠg‹( €€˜˜‚Q€ ‚’a<‹ö‹. ,€Ā€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1g‹'Œ1ļ’’’’’’’’:’’’’'ŒåŽė±ö‹: B€c€†Ų”Q€€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€ ‚’ØkåŽ= H€×€†Ų”Q€‚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=1’’’’’’’’;’’’’öĆė±åŽ Ą: B€c€†Ų”Q€€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 ĄåŽ+8Ą( €€˜˜‚Q€ ‚’ß ĄWĀ@ N€æ€†Ų”Q€‚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.Ÿj8ĄöĆ5 8€Õ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’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.1WĀ'Ä1ī’’’’’’’’<’’’’'ÄäĘė±öĆÅ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+'Ä=Å( €€˜˜‚Q€ ‚’§jÅäĘ= H€Õ€†Ų”Q€‚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=ÅĒ1’’’’’’’’=’’’’ĒčĖė±äĘČ: B€c€†Ų”Q€€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+Ē+Č( €€˜˜‚Q€ ‚’ŽČIŹ@ N€½€†Ų”Q€‚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.Ÿj+ČčĖ5 8€Õ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’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.1IŹĢ1“’’’’’’’’>’’’’Ģ{Īė±čĖĶ: B€c€†Ų”Q€€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+Ģ/Ķ( €€˜˜‚Q€ ‚’LĶ{Ī; D€#€†Ų”Q€‚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/ͬĪ1-’’’’’’’’?’’’’¬Īė±{Ī—Ļ: B€c€†Ų”Q€€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+¬ĪĀĻ( €€˜˜‚Q€ ‚’3š—ĻC T€į€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚ĀĻ{Ī‚‚‚‚’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 defaultćĀĻ2 2€Ē€†Ų”Q€‚‚‚‚‚‚‚‚‚’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.1G1M’’’’’’’’@’’’’Gcė±2: B€c€†Ų”Q€€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+G]( €€˜˜‚Q€ ‚’Ė2c; D€—€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 losses1]”1Ü’’’’’’’’A’’’’”? ė±c: B€c€†Ų”Q€€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+”Ŗ( €€˜˜‚Q€ ‚’ßČ ? L€æ€†Ų”Q€‚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.=Ŗ < F€€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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:Č ? ) "€"€†Ų”Q€‚’the Main menu.1 p 1 ’’’’’’’’B’’’’p Iė±? [ : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+p † ( €€˜˜‚Q€ ‚’Ɖ[ I: B€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’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† z1g’’’’’’’’C’’’’z®Dė±Iq@: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 54zq@I0-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+zœ@( €€˜˜‚Q€ ‚’Ōq@®B> J€©€†Ų”Q€‚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 theĘœ@®D: B€€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’default temperature value.STEP 5Select the desired outlet species (outlet working fluid) or go with the defaultspecies.STEP 6Enter the desired outlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 7Click on the Calculate button to start the calculation of mixing outletvalues for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1®BßD1Ą’’’’’’’’D’’’’ßDnFė±®DŹE: B€c€†Ų”Q€€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+ßDõE( €€˜˜‚Q€ ‚’yKŹEnF. ,€–€†Ų”Q€‚€‚‚’Compressible FlowThis section provides analysis of compressible flow.1õEŸF1R’’’’’’’’E’’’’ŸFĄHė±nFŠG: B€c€†Ų”Q€€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+ŸFµG( €€˜˜‚Q€ ‚’ ӊGĄH8 >€§€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Velocity of SoundThis section provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1µGńH15’’’’’’’’F’’’’ńHõKė±ĄHÜI: B€c€†Ų”Q€€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+ńHJ( €€˜˜‚Q€ ‚’ī²ÜIõK< F€e€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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.1J&L1M’’’’’’’’G’’’’&LBNė±õKM: B€c€†Ų”Q€€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+&L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1 J€Ļ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Mach NumberSTEP 1Sel‰OŗBNect 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:‰Oō) "€"€†Ų”Q€‚’the Main menu.1ŗ%‚1’’’’’’’’I’’’’%‚öƒė±ōƒ: B€c€†Ų”Q€€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+%‚;ƒ( €€˜˜‚Q€ ‚’»‹ƒöƒ0 .€€†Ų”Q€‚€‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1;ƒ'„1Š’’’’’’’’J’’’’'„€†ė±öƒ…: B€c€†Ų”Q€€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€ ‚’C …€†8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’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=…±†1I’’’’’’’’K’’’’±†Ɋė±€†œ‡: B€c€†Ų”Q€€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+±†LJ( €€˜˜‚Q€ ‚’*źœ‡ń‰@ N€Õ€†Ų”Q€‚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 stagnationتLJɊ. *€U€†Ų”Q€‚‚‚‚‚’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.1ń‰śŠ1~’’’’’’’’L’’’’śŠGė±ÉŠå‹: B€c€†Ų”Q€€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+śŠŒ( €€˜˜‚Q€ ‚’7’å‹G8 >€’€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’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 constant1Œx1Ł’’’’’’’’M’’’’xžĮė±GcŽ: B€c€†Ų”Q€€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+xŽŽ( €€˜˜‚Q€ ‚’0ņcŽŹĄ> J€å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 theŽŽŹĄG 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 staticŌ¦ŽŽžĮ. *€M€†Ų”Q€‚‚‚‚‚’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.1ŹĄĻĮ1ˆ’’’’’’’’N’’’’ĻĮ&Äė±žĮŗĀ: B€c€†Ų”Q€€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+ĻĮåĀ( €€˜˜‚Q€ ‚’A ŗĀ&Ä8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’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 constant1åĀWÄ1T’’’’’’’’O’’’’WÄzČė±&ÄBÅ: B€c€†Ų”Q€€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+WÄmÅ( €€˜˜‚Q€ ‚’)ėBÅ–Ē> J€×€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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,äµmÅzČ/ ,€k€†Ų”Q€‚‚‚‚‚‚’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–Ē«Č1M’’’’’’’’P’’’’«ČĒĖė±zČ–É: B€c€†Ų”Q€€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+«ČĮÉ( €€˜˜‚Q€ ‚’Ź–ÉĒĖ< F€•€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 constant1ĮÉųĖ1Y’’’’’’’’Q’’’’ųĖ“ė±ĒĖćĢ: B€c€†Ų”Q€€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+ųĖĶ( €€˜˜‚Q€ ‚’ ĢćĢĻ> J€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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_Ķ“1 0€æ€†Ų”Q€‚‚‚‚‚‚‚‚’Click on the Calculate button to start the calculation of inlet Machnumber, inlet static temperature, inlet static pressure, outlet Machnumber, outlet velocity, outlet static tempeĻ“ĒĖrature, 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.1Ļå1Œ’’’’’’’’R’’’’å@뱓Š: B€c€†Ų”Q€€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+åū( €€˜˜‚Q€ ‚’E Š@8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: DiffuserThis subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1ūq1F’’’’’’’’S’’’’q†ė±@\: B€c€†Ų”Q€€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‡( €€˜˜‚Q€ ‚’Ż\¢> J€»€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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,䵇†/ ,€k€†Ų”Q€‚‚‚‚‚‚’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¢·1Į’’’’’’’’T’’’’·G 뱆¢: B€c€†Ų”Q€€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+·Ķ( €€˜˜‚Q€ ‚’zA¢G 9 @€ƒ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’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 constant1Ķx 1’’’’’’’’U’’’’x cė±G c : B€c€†Ų”Q€€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+x Ž ( €€˜˜‚Q€ ‚’.šc ¼ > J€į€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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§pŽ c7 <€į€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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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