?_’’’’c›ofl…’’’’’’’’’’’’9 ¶pB-#B[+JD[+’’uĒBI’’’’“ĒB-#EV[+^D[+’’ņuĒBI’’’’buĒBĒB3) I[+hhŒŒ=@\\ 0 3 ł ’’-#’’’’[[+cD[+’’&z-#’’ē[+ļR[+’’ą}Ē?T6T’’’’ 1’’’’=1 ’’’’’’’’=ƒŃ é° &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.com]7=ƒ& €n€°°€‚’Power and Propulsion SystemsAnalysis 1.1 - TutorialŸ&Ÿ} Ȁ?€°˜ć\ŖÓP€‰€‚ćS?€‰€‚ć$ēdI€‰€‚ćĢ’§n€‰€‚ć\–€‰€‚ćf¢v“€‰€‚怉€‚’Program DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPower Cycles@ƒß2 4€€˜˜€ƒć°€ ‰€ ‚’CarnotR!Ÿ11 2€B€€ƒƒć²ś€ ‰€ ‚’Running - Carnot CycleAßr2 4€€°˜€ƒć±€ ‰€ ‚’BraytonI1»3 6€,€˜˜€ƒƒćn«€ ‰€ ‚’Power (Ideal)e3r 2 4€f€€ƒƒƒćœG¾€ ‰€ ‚’Running - Brayton Cycle: Power (Ideal)J»j0 0€4€°˜€ ƒƒćp«‰€ ‚’Propulsion (Ideal)j8 Ō2 4€p€€ ƒƒƒćņG¾€ ‰€ ‚’Running - Brayton Cycle: Propulsion (Ideal)=j/ .€€°˜€ ƒć²‰€ ‚’RankineS"Ōd1 2€D€€ ƒƒćū€ ‰€ ‚’Running - Rankine CycleT&ø. ,€L€°˜ć€‰€‚’Power Cycle Components/Processesm,d%A R€X€˜˜€ƒćé€ ‰€ ‚€ ƒƒćęB߉€ ‚’CompressionIsentropic (Ideal)h6ø2 4€l€€ ƒƒƒćÄ<€%€ ‰€ ‚’Running - Compression: Isentropic (Ideal)@%Ķ/ .€"€°˜€ ƒćꉀ ‚’Combustion@ 0 0€ €˜˜€ ƒƒćJ߉€ ‚’Coal/Oil]+Ķj2 4€V€€ ƒƒƒćWs%€ ‰€ ‚’Running - Combustion: Coal/Oil; „0 0€€°˜€ ƒƒć J߉€ ‚’GasX&jż2 4€L€€ ƒƒƒć‚s%€ ‰€ ‚’Running - Combustion: Gas?„</ .€ €°˜€ ƒć뉀 ‚’ExpansionJż†0 0€4€˜˜€ ƒƒćXQ߉€ ‚’Isentropic (Ideal)f4<ģ2 4€h€€ ƒƒƒćź©‚%€ ‰€ ‚’Running - Expansion: Isentropic (Ideal)d(†P < H€P€°˜ć€‰€‚€ ƒć#&‰€ ‚’Compressible FlowMach NumberQ ģ” 1 2€@€€ ƒƒćh€ ‰€ ‚’Running - Mach Number< P Ż / .€€°˜€ ƒć%&‰€ ‚’NozzleL” ) 1 2€6€€ ƒƒćYh€ ‰€ ‚’Running - NozzleBŻ k / .€&€°˜€ ƒć&&‰€ ‚’Normal ShockR!) ½ 1 2€B€€ ƒƒć„h€ ‰€ ‚’Running - Normal Shock>k ū / .€€°˜€ ƒć'&‰€ ‚’DiffuserN½ I 1 2€:€€ ƒƒćÆh€ ‰€ ‚’Running - Diffuser< ū … / .€€°˜€ ƒć(&‰€ ‚’ThrustLI Ń 1 2€6€€ ƒƒćŚh€ ‰€ ‚’Running - Thrust1…  1 ’’’’’’’’’’’’ ēDė±Ń ķ : 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€ ‚’Ėķ < F€—€€‚€‚€ €‚€ €‚‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power and Propulsion Systems Analysis, that quickly andreliably analyzes power cycles, power cycle components/processes andcompressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofpower and propulsion systems. It should provide you with the opportunityŹ =AH ^€•€€‚‚‚‚‚€ €€ €‚‚€ ‚€ƒ‚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=AŃ 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.Power CyclesCarnotBrayton (Power and Propulsion)RankinePower Cycle Components/ProcessesažBK d€-€€ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ƒ‚ƒ‚ƒ‚ƒ‚’CompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowMach NumberNozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:h:=AC. ,€t€†üE”€ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ߞBD, &€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„CēD1 0€K€€‚€ ‚€‚‚‚‚‚‚’Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1DE1q’’’’’’’’’’’’EXLė±ēDF: 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€ ‚’ ĖF7H> 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:"ą.FYJB 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’·7HXLH ^€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 constant1YJ‰L1P’’’’’’’’’’’’‰LØOė±XLtM: 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+‰LŸM( €€˜˜‚Q€ ‚’ ĪtMØO; D€€†Ų”Q€‚€‚€ ‚€‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Power and Propulsion SystemsAnalysis program, the user needs to change one or more input valuesin order to calculate a new case. Input values are in boxes with whitebackground and can be changed by clicking on each individual box oreven by using the arrow keys and changing the current value. Outputvalues cannot be modified, changed by the user and they are in boxeswith black background.1ŸMŁO1W’’’’’’’’’’’’ŁO †ė±ØOŠ€: B€c€†Ų”Q€ŁOŠ€ØO€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+ŁOū€( €€˜˜‚Q€ ‚’5óŠ€0ƒB R€ē€†Ų”Q€‚€‚€ €‚‚‚‚€ €‚‚‚‚’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 thisAńū€q…P n€ć€†Ų”Q€‚€ €€ €‚€ €€ €‚‚‚‚‚€ €‚‚’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, thenšm0ƒ †- *€Ś€†Ų”Q€ €‚‚’Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1q…<†1"’’’’’’’’’’’’<†-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+<†R‡( €€˜˜‚Q€ ‚’L'‡ž‡- *€>€†Ų”Q€‚€‚’Suggestion/Evaluation FormÜR‡²ˆ8 >€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‘]ž‡C‰4 8€ŗ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:Q(²ˆ”‰) "€P€ †Ų”Q€ ‚’Power and Propulsion Systems Analysis™[C‰-Š> L€¶€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Quality:Usefulness:Possible areas of improvement:Other suggestions:1”‰^Š1j’’’’’’’’’’’’^Š—ė±-ŠI‹: 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+^Št‹( €€˜˜‚Q€ ‚’ ÜI‹”D 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 andĻt‹—4 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 software1”Č1³’’’’’’’’’’’’ȏVĆė±—æĄ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒČæĄ—‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ȏźĄ( €€˜˜‚Q€ ‚’ßæĄ’Ā6 :€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.źĄVĆ) "€\€†Ų”Q€‚’steam table calculations are not available.1’‡Ć1’’’’’’’’’’’’‡ĆęÅė±VĆrÄ: 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+‡ĆÄ( €€˜˜‚Q€ ‚’IrÄęÅ9 @€!€†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ÄĘ1„’’’’’’’’ ’’’’ʋÉļ²ęÅĒ= 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+Ę1Ē( €€˜˜‚Q€ ‚’ āĒQÉ> 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:1Ē‹É) "€"€†Ų”Q€‚’the Main menu.1QɼÉ1‡’’’’’’’’ ’’’’¼ÉĢ뱋ɧŹ: 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+¼ÉŅŹ( €€˜˜‚Q€ ‚’@§ŹĢ9 @€€†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 constant1ŅŹCĢ1—’’’’’’’’ ’’’’CĢ©Ļė±Ģ.Ķ: 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+CĢYĶ( €€˜˜‚Q€ ‚’Ł.ĶoĻ= 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:YĶ©Ļ) "€"€†Ų”Q€‚’the Main menu.1oĻŚĻ1’’’’’’’’ ’’’’ŚĻ7뱩ĻŃ: B€c€†Ų”Q€ŚĻѩπƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŚĻü( €€˜˜‚Q€ ‚’;Ń78 >€€†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 constant1üh1”’’’’’’’’ ’’’’hĖė±7S: 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+h~( €€˜˜‚Q€ ‚’ÖS‘= 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 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:~Ė) "€"€†Ų”Q€‚’the Main menu.1‘ü1’’’’’’’’’’’’üŚ ė±Ėē: 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+ü( €€˜˜‚Q€ ‚’(ķē: ; 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 vŚ * $€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:  1«’’’’’’’’’’’’ … ė±Ś 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+ ! ( €€˜˜‚Q€ ‚’d,ö … 8 >€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±… ” : 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 ( €€˜˜‚Q€ ‚’Ș” ”0 .€1€†Ų”Q€‚€‚‚‚’Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1Ģ Å1h’’’’’’’’’’’’Å¢Aė±”°: 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€ ‚’»ƒ°¢A8 >€€†Ų”QŪ¢A”€‚€‚‚‚‚‚‚‚‚‚‚‚’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 Properties1ŪÓA1Š’’’’’’’’’’’’ÓA,Eė±¢A¾B: 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+ÓAéB( €€˜˜‚Q€ ‚’ ̾BņD= 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 values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back to:éB,E) "€"€†Ų”Q€‚’the Main menu.1ņD]E1W’’’’’’’’’’’’]EƒHė±,EHF: 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+]EsF( €€˜˜‚Q€ ‚’ŅHFƒH> 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.1sF“H1©’’’’’’’’’’’’“H,K뱃HŸI: 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+“HŹI( €€˜˜‚Q€ ‚’b,ŸI,K6 :€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 Properties1ŹI]K1Y’’’’’’’’’’’’]K…Nė±,KHL: 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+]KsL( €€˜˜‚Q€ ‚’ÕHL…N= 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.1sL¶N1 ’’’’’’’’’’’’¶Nk€ė±…N”O: 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+¶NĢO( €€˜˜‚Q€ ‚’“e”Ok€. ,€Ź€†Ų”Q€‚€‚‚’PowerĢOk€…N CyclesThis section provides analysis of a few power cycles (Carnot, Brayton and Rankine).1ĢOœ€1Ī’’’’’’’’’’’’œ€9ƒė±k€‡: 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€²( €€˜˜‚Q€ ‚’‡N‡9ƒ9 @€€†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.1²jƒ1P’’’’’’’’’’’’jƒ‰†ė±9ƒU„: 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+jƒ€„( €€˜˜‚Q€ ‚’ ĢU„‰†= 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.1€„ŗ†1’’’’’’’’’’’’ŗ†‰ˆ뱉†„‡: 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†Ї( €€˜˜‚Q€ ‚’¹‰„‡‰ˆ0 .€€†Ų”Q€‚€‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1Їŗˆ1’’’’’’’’’’’’ŗˆŒ뱉ˆ„‰: 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+ŗˆЉ( €€˜˜‚Q€ ‚’Ū„‰ę‹; 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.©ЉŒ* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1ꋥŒ1v’’’’’’’’’’’’ĄŒĀė±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+ĄŒ֍( €€˜˜‚Q€ ‚’@«"Ą? 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֍"ĄŒ go with the defaultä«֍Ā9 @€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.1"Ą7Ā1’’’’’’’’’’’’7Ā Ęė±Ā"Ć: 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+7ĀMĆ( €€˜˜‚Q€ ‚’Ś"ĆbÅ; 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 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.©MĆ Ę* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1bÅ<Ę1j’’’’’’’’’’’’<ĘuĖė± Ę'Ē: 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+<ĘRĒ( €€˜˜‚Q€ ‚’?'Ē‘É? 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«RĒuĖ9 @€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.1‘ɦĖ1’’’’’’’’’’’’¦ĖĻė±uĖ‘Ģ: 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+¦Ė¼Ģ( €€˜˜‚Q€ ‚’9ż‘ĢõĪ< 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›q¼ĢĻ* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1õĪĮĻ1ģ’’’’’’’’’’’’ĮĻ 뱐Ļø: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’EngiĮĻøĻneering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĮĻć( €€˜˜‚Q€ ‚’Eø(? 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 defaultä«ć 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.1(=1’’’’’’’’ ’’’’=& 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€ ‚’8ü(‹< 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›qS& * $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1‹W 1o’’’’’’’’!’’’’W •ė±& B : 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+W m ( €€˜˜‚Q€ ‚’DB ± ? 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«m •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.1± Ę1’’’’’’’’"’’’’Ę}A뱕±: 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+ĘÜ( €€˜˜‚Q€ ‚’•[±}A: B€·€†Ų”QÜ}A•€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’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.1Ü®A1ä’’’’’’’’#’’’’®AaEė±}A™B: 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+®AÄB( €€˜˜‚Q€ ‚’Ó™BÓD< 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.STEP 4Click on the Calculate button to start the calculation of the Rankine cycleoutput values for the chosen input values.ŽbÄBaE, (€Ä€†Ų”Q€‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1ÓD’E1Ū’’’’’’’’$’’’’’E 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 ²Ą.Å< 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 desired mobility value or go with the default mobility value.STEP 10Click on the Calculate button to start the calculation of the Magnetohydrodynamics cycle output values for the chosen input values.dę¾Å, (€Č€†Ų”Q€‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1.ÅļÅ1Ā’’’’’’’’*’’’’ļÅ€Čė±¾ÅŚĘ: 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+ļÅĒ( €€˜˜‚Q€ ‚’ߌĘČ/ ,€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:mDĒ€Č) "€ˆ€†Ų”Q€‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1ȱČ1’’’’’’’’+’’’’±ČĶė±€ČœÉ: 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+±ČĒÉ( €€˜˜‚Q€ ‚’ įœÉēĖ? 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(öĒÉĶ2 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.1ēĖ@Ķ1’’’’’’’’,’’’’@ĶĻė±Ķ+Ī: 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+@ĶVĪ( €€˜˜‚Q€ ‚’Į‘+ĪĻ0 .€#€†Ų”Q€‚€‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1VĪHĻ1Ś’’’’’’’’-’’’’HĻżė±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@engineeriHĻ?Ļng-4e.comWeb Site:http://www.engineering-4e.com+HĻj( €€˜˜‚Q€ ‚’“e?ż. ,€Ź€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1j.1ō’’’’’’’’.’’’’.ńė±ż: 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+.D( €€˜˜‚Q€ ‚’­pń= 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.1D"1Ų’’’’’’’’/’’’’"Éė±ń : 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+"8( €€˜˜‚Q€ ‚’ Ē AB 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 5ˆU8É3 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.1Aś1ó’’’’’’’’0’’’’ś¼ ė±Éå : 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+ś ( €€˜˜‚Q€ ‚’¬oå ¼ = 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.1 ķ 1-’’’’’’’’1’’’’ķ Ÿ@ė±¼ Ų : 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€ ‚’ĘŲ  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 5ˆU Ÿ@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 an Ÿ@¼ d 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 Š@1×’’’’’’’’2’’’’Š@vC뱟@»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+Š@ęA( €€˜˜‚Q€ ‚’S»AvC= 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 compression1ęA§C1 ’’’’’’’’3’’’’§CHė±vC’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+§C½D( €€˜˜‚Q€ ‚’Až’DžFC 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 defaultę½DH2 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.1žFGH1Ų’’’’’’’’4’’’’GHīIė±H2I: 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+GH]I( €€˜˜‚Q€ ‚’‘c2IīI. ,€Ę€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1]IJ1©’’’’’’’’5’’’’J—Mė±īI K: 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+J5K( €€˜˜‚Q€ ‚’Ł KMM? 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!5K—M) "€B€†Ų”Q€‚’Specific heat is not constant.1MMČM1q’’’’’’’’6’’’’ČM$„ė±—M³N: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ČMŽN( €€˜˜‚Q€ ‚’B³N,< F€ €†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes: Combustion:Coal/OilSTEP 1Enter the desired fuel (coal or oil) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click onŽN,—M theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.%ėŽNQƒ: B€×€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Furthermore, click on the fuel Normalize button one more time tocalculate the new stoichiometry value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired oxidant to fuel ratio ( > 1) or go with the default oxidantto fuel ratio.STEP 6Click on the Calculate button to start the calculation of combustion gasÓ¦,$„- (€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.1QƒU„1œ’’’’’’’’7’’’’U„Ą‡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+U„k…( €€˜˜‚Q€ ‚’ Ģ@…v‡? 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!k…Ą‡) "€B€†Ų”Q€‚’Specific heat is not constant.1v‡ń‡1x’’’’’’’’8’’’’ń‡8Žė±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+ń‡‰( €€˜˜‚Q€ ‚’7ś܈>‹= 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.%ė‰c: 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§>‹8Ž. *€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.1ciŽ1Ö’’’’’’’’9’’’’iŽĄė±8ŽT: 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+iŽ( €€˜˜‚Q€ ‚’aTĄ. ,€Ā€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis oĄ8Žf expansion.1KĄ1ļ’’’’’’’’:’’’’KĄ Ćė±Ą6Į: 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+KĄaĮ( €€˜˜‚Q€ ‚’Øk6Į Ć= 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.1aĮ:Ć1’’’’’’’’;’’’’:ĆČė± Ć%Ä: 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+:ĆPÄ( €€˜˜‚Q€ ‚’ß%ÄoĘ@ 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.ŸjPÄČ5 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.1oĘ?Č1ī’’’’’’’’<’’’’?ČüŹė±Č*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+?ČUÉ( €€˜˜‚Q€ ‚’§j*ÉüŹ= 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.1UÉ-Ė1’’’’’’’’=’’’’-Ė ė±üŹĢ: 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+-ĖCĢ( €€˜˜‚Q€ ‚’ŽĢaĪ@ 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.ŸjCĢ 5 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.aĪ üŹ1aĪ=1“’’’’’’’’>’’’’=Ÿė± (: 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€ ‚’L(Ÿ; 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 expansion1SŠ1’’’’’’’’?’’’’Š.뱟»: 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+Šę( €€˜˜‚Q€ ‚’3š»C T€į€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Expansion: IsothermalSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired turbine inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired turbine mass value or go with the defaultćę.2 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.1_1M’’’’’’’’@’’’’_{ ė±.J: 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+_u( €€˜˜‚Q€ ‚’ĖJ{ ; 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 losses1u¬ 1Ü’’’’’’’’A’’’’¬ c@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+¬ Ā ( €€˜˜‚Q€ ‚’ß— ą ? 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.=Ā )@< 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 thą )@{ e Exit button to go back to:ą c@) "€"€†Ų”Q€‚’the Main menu.1)@”@1 ’’’’’’’’B’’’’”@mCė±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+”@ŖA( €€˜˜‚Q€ ‚’ƉAmC: 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 losses1ŖAžC1Y’’’’’’’’C’’’’žCĘHė±mC‰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+žC“D( €€˜˜‚Q€ ‚’Ō‰DĘF> 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 theĘ“DĘH: 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.1ĘF÷H1Ą’’’’’’’’D’’’’÷H†Jė±ĘHāI: 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+÷H J( €€˜˜‚Q€ ‚’yKāI†J. ,€–€†Ų”Q€‚€‚‚’Compressible FlowThis section provides analysis of compressible flow.1 J·J1R’’’’’’’’E’’’’·JŲL뱆J¢K: 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+·JĶK( €€˜˜‚Q€ ‚’ Ó¢KŲL8 >€§€†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 constant1ĶK M15’’’’’’’’F’’’’ M€ė±ŲLōM: 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+ MN( €€˜˜‚Q€ ‚’ī²ōM€< 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 totheN€ŲL Main menu.1NJ€1M’’’’’’’’G’’’’J€f‚ė±€5: 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€`( €€˜˜‚Q€ ‚’Ī5f‚8 >€€†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`—‚1¦’’’’’’’’H’’’’—‚ †ė±f‚‚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€ ‚’%ē‚ƒŅ…> J€Ļ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Mach NumberSTEP 1Select the desired working fluid (specie) or go with the default value.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Enter the desired velocity value or go with the default velocity value.STEP 4Click on the Calculate button to start the calculation of Mach numbervalue for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:­ƒ †) "€"€†Ų”Q€‚’the Main menu.1Ņ…=†1’’’’’’’’I’’’’=†ˆė± †(‡: 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€ ‚’»‹(‡ˆ0 .€€†Ų”Q€‚€‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1S‡?ˆ1Š’’’’’’’’J’’’’?ˆ˜Šė±ˆ*‰: 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+?ˆU‰( €€˜˜‚Q€ ‚’C *‰˜Š8 >€€†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 constant1U‰Ɋ1I’’’’’’’’K’’’’ɊįŽ뱘Š“‹: 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+Ɋߋ( €€˜˜‚Q€ ‚’*ź“‹ Ž@ 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 stagnationŲŖß‹įŽ. *€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.1 Ž1~’’’’’’’’L’’’’nĮė±įŽ 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 ĄįŽ+7Ą( €€˜˜‚Q€ ‚’7’ ĄnĮ8 >€’€†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 constant17ĄŸĮ1K’’’’’’’’M’’’’ŸĮ¹Åė±nĮŠĀ: 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+ŸĮµĀ( €€˜˜‚Q€ ‚’0ņŠĀåÄ> 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 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 staticŌ¦µĀ¹Å. *€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.1åÄźÅ1ˆ’’’’’’’’N’’’’źÅAČė±¹ÅÕĘ: 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+źÅĒ( €€˜˜‚Q€ ‚’A ÕĘAČ8 >€€†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 constant1ĒrČ1T’’’’’’’’O’’’’rČ•Ģė±AČ]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+rČˆÉ( €€˜˜‚Q€ ‚’)ė]ɱĖ> 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,䵈É•Ģ/ ,€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±ĖĘĢ1M’’’’’’’’P’’’’ĘĢ 뱕̱Ķ: 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+ĘĢÜĶ( €€˜˜‚Q€ ‚’Ź±Ķ < 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 constantÜĶ •Ģ1ÜĶ=1ę’’’’’’’’Q’’’’=ķė± (: 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(]> 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_Sķ1 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 temperature, and outlet staticpressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1]1Œ’’’’’’’’R’’’’yė±ķ : 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( €€˜˜‚Q€ ‚’E  y8 >€€†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 constant14Ŗ1F’’’’’’’’S’’’’Ŗæ ė±y•: 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+ŖĄ( €€˜˜‚Q€ ‚’Ż•Ū > 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,䵥æ / ,€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.1Ū š 1Į’’’’’’’’T’’’’š €뱿 Ū : 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+š  ( €€˜˜‚Q€ ‚’zAŪ €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 constant1 ±1Ą’’’’’’’’U’’’’±ØCė±€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+±Ē( €€˜˜‚Q€ ‚’.šœB> J€į€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚ĒB€‚‚‚‚’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§pĒØC7 <€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 on the Exit button to go back tothe Main menu.1BŁC1]’’’’’’’’V’’’’ŁCD,ØCD) "€€†Ų”Q€‚’1ŁC’’’’1’’’’’’’’W’’’’’’’’’’’’ 22wT1Helv&ˆC‹v 9\'~év’Tms RmnFō^_‹å]ŹU‹Symbol^‰^ų&öt"&‹CourierŲ-Ś@Ä^ &Times New Romanč-@Arial&ĒGƒFÄ^ƒMS Serif‰Fō‰VöŠFō%MS Sans Serif&‰GŠTimes‰O ŠN÷ƒį ŠéŠé&HelveticaÓź&‰W ĄtSystemt$&‹&‹WŃźŃCourier New‰G&‰WƒRoman&‹Ńč-@Ä^ &‰GScriptƒFėÄ^ +Ą&ModernöFöt[Ä^&öMarlett@Ä^ &‰GƒFArial CE*ä-@Ä^ &‰GArial CYR^™RPÄv &‹DArial Greek<9¢Ä^ &‰Arial TURöFöt[ÄArial Balticg*æ&‹G)Courier New CE)FŽF Courier New CYR-„‹FCourier New GreekWVCourier New TURé–Courier New BalticƒLucida Console|Lucida Sans UnicodeTimes New Roman CETimes New Roman CYRTimes New Roman GreTimes New Roman TURTimes New Roman BalWingdingsĮ‹Ų&€?wƒVerdanaų¹”©ŽŁ^_‹å]ŹArial Black‹ū&€?uComic Sans MSv &ŠŽGeorgiaÄ^&öt#&‹Franklin Gothic MedPalatino Linotype@Tahoma&ĒDƒFŽF Trebuchet MSt&‹ŃčWebdingsėV&ŠŠč*Estrangelo EdessaŠGautami’FÄ^&‹&‹WLatha&‰TƒF&€ŽFžHanzel Condensed· ĄHanzel Extended’všHanzel Ž0&ĒŌ ŽHanzel ThinŹ U‹ģŽHanzel Wide&‹G 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