?_v’’’’y“f]l… € ‰€ ‚’Temperature - Pressure\+Š61 2€V€€ƒƒćŒ€ ‰€ ‚’Running - Temperature - PressureMŚƒ2 4€6€°˜€ƒć? € ‰€ ‚’Enthalpy - PressureY(6Ü1 2€P€€ ƒƒć·€ ‰€ ‚’Running - Enthalpy - PressureLƒ(2 4€4€°˜€ƒć@ € ‰€ ‚’Entropy - PressureX'Ü€1 2€N€€ƒƒćā€ ‰€ ‚’Running - Entropy - Pressure1(±1‚’’’’’’’’’’’’± ė±€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€ ‚’Eœ = H€€€‚€‚€ €‚€ €‚‚‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Physical Properties, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunityto more quickly and effectively do your work, explore more options, save×Ē* G \€Æ€€‚‚‚‚€ €€ €‚‚€ ‚€ƒ‚ƒ‚ƒ‚‚€ ‚’time 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 PressureEntropy and PressureHardware Requirements and Software Compatibilitye ¹ * $€Ź€€ƒ‚ƒ‚ƒ‚ƒ‚’80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:h:* ! . ,€t€†üE”€ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ß¹ , , &€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„!  1 0€K€€‚€ ‚€‚‚‚‚‚‚’Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1, 3 1q’’’’’’’’’’’’3 Dė± : 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+3 I( €€˜˜‚Q€ ‚’ Ė^@> 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 afI^@ orementioned engineering calculations are valid underthe following assumptions:"ąI€BB 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’·^@DH ^€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 constant1€B°D1=’’’’’’’’’’’’°D¼Gė±D›E: 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+°DĘE( €€˜˜‚Q€ ‚’ö»›E¼G; D€w€†Ų”Q€‚€‚€ €‚‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Physical Properties program,the user needs to change one or more input values in order tocalculate a new case. Input values are in boxes with whitebackground and can be changed by clicking on each individualbox or even by using the arrow keys and changing the current value.Output values cannot be modified, changed by the user and theyare in boxes with black background.1ĘEķG1W’’’’’’’’’’’’ķGNė±¼GŲH: 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+ķGI( €€˜˜‚Q€ ‚’5óŲH8KB 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 thisAńIyMP 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, thenšm8KN- *€Ś€†Ų”Q€ €‚‚’Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1yMDN1’’’’’’’’’’’’DN-‚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+DNZO( €€˜˜‚Q€ ‚’L/O¦O- *€>€†Ų”Q€‚€‚’Suggestion/Evaluation FormÜZOʀ8 >€¹€ †Ų”Q€‚‚€ ‚€‚‚‚‚‚‚’Please FAX or Mail This Suggestio¦OʀNn/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‘]¦OW4 8€ŗ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:?ʀ–) "€,€ †Ų”Q€ ‚’Physical Properties—ZW-‚= J€“€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Quality:Usefulness:Possible areas of improvement:Other suggestions:1–^‚1j’’’’’’’’’’’’^‚—‡ė±-‚Iƒ: 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+^‚tƒ( €€˜˜‚Q€ ‚’ ÜIƒ”…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 andĻtƒ—‡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”…ȇ1³’’’’’’’’’’’’ȇJ‹ė±—‡³ˆ: 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+ȇŽˆ( €€˜˜‚Q€ ‚’ß³ˆóŠ6 :€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.ŽˆJ‹) "€\€†Ų”Q€‚’steam table calculations are not available.1óŠ{‹1’’’’’’’’’’’’{‹Śė±J‹fŒ: 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€ ‚’IfŒŚ9 @€!€†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‘Œ Ž1„’’’’’’’’ ’’’’ Ž‹Įļ²ŚśŽ= 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+ Ž%( €€˜˜‚Q€ ‚’ āśŽQĮ> J€Å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Properties: Temperature - PressureSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired temperature valu%QĮŚe 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:%‹Į) "€"€†Ų”Q€‚’the Main menu.1QĮ¼Į1‡’’’’’’’’ ’’’’¼ĮÄė±‹Į§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+¼ĮŅĀ( €€˜˜‚Q€ ‚’@§ĀÄ9 @€€†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 constant1ŅĀCÄ1—’’’’’’’’ ’’’’CÄ©Ēė±Ä.Å: 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+CÄYÅ( €€˜˜‚Q€ ‚’Ł.ÅoĒ= 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:YÅ©Ē) "€"€†Ų”Q€‚’the Main menu.1oĒŚĒ1‚’’’’’’’’ ’’’’ŚĒ+Źė±©ĒÅČ: 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+ŚĒšČ( €€˜˜‚Q€ ‚’;ÅČ+Ź8 >€€†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 constant1šČ\Ź1”’’’’’’’’ ’’’’\ŹæĶė±+ŹGĖ: 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+\ŹrĖ( €€˜˜‚Q€ ‚’ÖGĖ…Ķ= 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:rĖæĶ) "€"€†Ų”Q€‚’the Main menu.1…ĶšĶ1 ’’’’’’’’’’’’šĶŚė±æĶŪĪ: 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+šĶĻ( €€˜˜‚Q€ ‚’(ķŪĪ:; 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 foĻ:æĶllows: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 vĻŚ* $€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±Śö: 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.1ĢÅ1’’’’’’’’’’’’Å– 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+ÅŪ( €€˜˜‚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 Properties1ŪĒ 1Š’’’’’’’’’’’’Ē  ė±– 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+Ē Ż ( €€˜˜‚Q€ ‚’ Ģ² ę = 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:Ż  ) "€"€†Ų”Q€‚’the Main menu.1ę Q 1ž’’’’’’’’’’’’Q ƒ@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 g( €€˜˜‚Q€ ‚’Ņ<ƒ@> 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 thegƒ@  chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1g“@1©’’’’’’’’’’’’“@,Cė±ƒ@ŸA: 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+“@ŹA( €€˜˜‚Q€ ‚’b,ŸA,C6 :€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 Properties1ŹA]C1Y’’’’’’’’’’’’]C…Fė±,CHD: 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+]CsD( €€˜˜‚Q€ ‚’ÕHD…F= 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.1sD¶F1 ’’’’’’’’’’’’¶FHė±…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+¶FĢG( €€˜˜‚Q€ ‚’Ĕ”GH0 .€)€†Ų”Q€‚€‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1ĢGĮH1Ī’’’’’’’’’’’’ĮH^Kė±H¬I: 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+ĮH×I( €€˜˜‚Q€ ‚’‡N¬I^K9 @€€†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.1×IK1P’’’’’’’’’’’’K®Nė±^KzL: 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„L( €€˜˜‚Q€ ‚’ ĢzL®N= 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„LßN1~’’’’’’’’’’’’ßNŀė±®NŹO: 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+ßN €( €€˜˜‚Q€ ‚’ŹO €®N¹‰ŹOŀ0 .€€†Ų”Q€‚€‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1 €ö€1’’’’’’’’’’’’ö€Ė„ė±Å€į: 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+ö€ ‚( €€˜˜‚Q€ ‚’Ūį"„; 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.© ‚Ė„* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1"„ü„1k’’’’’’’’’’’’ü„6Šė±Ė„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+ü„†( €€˜˜‚Q€ ‚’@ē…Rˆ? 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䫆6Š9 @€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.1RˆgŠ1’’’’’’’’’’’’gŠ;Žė±6ŠR‹: 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+gŠ}‹( €€˜˜‚Q€ ‚’ŚR‹’; 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.©}‹;Ž* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1’lŽ1š’’’’’’’’’’’’lŽ±Ćė±;ŽW: 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+lŽ‚( €€˜˜‚Q€ ‚’?WĶĮ? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Power (Real)STEP 1Sel‚ĶĮ;Žect 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«‚±Ć9 @€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.1ĶĮāĆ1’’’’’’’’’’’’āĆĢĒė±±ĆĶÄ: 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+āĆųÄ( €€˜˜‚Q€ ‚’9żĶÄ1Ē< 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›qųÄĢĒ* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.11ĒżĒ1p’’’’’’’’’’’’żĒ<Ķė±ĢĒčČ: 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+żĒÉ( €€˜˜‚Q€ ‚’EčČXĖ? 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«É<Ķ9 @€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.1XĖmĶ1š’’’’’’’’ ’’’’mĶbė±<ĶXĪ: 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+mĶƒĪ( €€˜˜‚Q€ ‚’8üXĪĒ< 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 ValƒĪĒ<Ķues:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine power›qƒĪb* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1Ē“1o’’’’’’’’!’’’’“Ńė±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+“©( €€˜˜‚Q€ ‚’D~ķ? 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«©Ń9 @€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.1ķ1Ü’’’’’’’’"’’’’­ ė±Ńķ: 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€ ‚’•[ķ­ : 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.1Ž 1ä’’’’’’’’#’’’’Ž ‘ ė±­ 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+Ž ō ( €€˜˜‚Q€ ‚’ÓÉ  < 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.Žbō ‘ , (€Ä€†Ų”Q€‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1 Ā 1¢’’’’’’’’$’’’’Ā xAė±‘ ­: 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 Ų( €€˜˜‚Q€‚’*ń­A9 @€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 CylindersŲA‘ , 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?ŲxA+ &€~€†Ų”Q€‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1A©A1·’’’’’’’’%’’’’©A/Hė±xA”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+©AæB( €€˜˜‚Q€ ‚’)ź”BčD? 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!åæB G< 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&ōčD/H2 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 G`H1ń’’’’’’’’&’’’’`H Lė±/HKI: 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+`HvI( €€˜˜‚Q€ ‚’2łKIØK9 @€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, FuelxLvI L, (€˜€†Ų”Q€‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1ØKQL1_’’’’’’’’'’’’’QLł‚ė± L 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 ՈQ< 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.d ‹į, (€Č€†Ų”Q€‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1QŽ1Č’’’’’’’’*’’’’ŽÆĄė±įżŽ: 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+Ž(( €€˜˜‚Q€ ‚’ßżŽBĄ/ ,€æ€€‚€‚‚‚‚‚‚‚‚’Power Cycles: Fuel CellThis subsection provides analysis of the Fuel Cell cycle.Input Values:Fuel, Fuel Inlet Temperature, Oxidant (O2) Inlet Temperature,Fuel F(BĄįlow Rate, Product Outlet TemperatureOutput Values:mD(ÆĄ) "€ˆ€†Ų”Q€‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1BĄąĄ1’’’’’’’’+’’’’ąĄ>Åė±ÆĄĖĮ: 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+ąĄöĮ( €€˜˜‚Q€ ‚’ įĖĮÄ? 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(ööĮ>Å2 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.1ÄoÅ1’’’’’’’’,’’’’oÅ]Ēė±>ÅZĘ: 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+oÅ…Ę( €€˜˜‚Q€ ‚’ŲØZĘ]Ē0 .€Q€†Ų”Q€‚€‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1…ĘŽĒ1Ś’’’’’’’’-’’’’ŽĒ7Éė±]ĒyČ: 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+ŽĒ¤Č( €€˜˜‚Q€ ‚’“eyČ7É. ,€Ź€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1¤ČhÉ1ō’’’’’’’’.’’’’hÉ+Ģė±7ÉSŹ: 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+hÉ~Ź( €€˜˜‚Q€ ‚’­pSŹ+Ģ= 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.1~Ź\Ģ1«’’’’’’’’/’’’’\Ģė±+ĢGĶ: 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+\ĢrĶ( €€˜˜‚Q€ ‚’ ĒGĶ{ĻB 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 5ˆUrĶ3 4€«€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass flow rate value or go with the defaultmass flo{Ļ+Ģw 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{Ļ@1ó’’’’’’’’0’’’’@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+@V( €€˜˜‚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.1V31×’’’’’’’’1’’’’3Łė±: 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+3I( €€˜˜‚Q€ ‚’ĘQB 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 5ˆUIŁ3 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.1Q 1×’’’’’’’’2’’’’ ° ė±Łõ : 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€ ‚’Sõ ° = 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 į 1Ą’’’’’’’’3’’’’į \@ė±° 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+į ÷ ( €€˜˜‚Q€ ‚’AžĢ 8C 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÷ \@2 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 done8\@°  with Steps 1 through 6, click on the Exit button to go back tothe Main menu.18@1Ų’’’’’’’’4’’’’@4Bė±\@xA: 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+@£A( €€˜˜‚Q€ ‚’‘cxA4B. ,€Ę€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1£AeB1©’’’’’’’’5’’’’eBŻEė±4BPC: 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+eB{C( €€˜˜‚Q€ ‚’ŁPC“E? 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!{CŻE) "€B€†Ų”Q€‚’Specific heat is not constant.1“EF1’’’’’’’’6’’’’F^Lė±ŻEłF: 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+F$G( €€˜˜‚Q€ ‚’BłFfI< F€ €†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes: Combustion:Coal/OilSTEP 1Enter the desired fuel (coal or oil) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.%ė$G‹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 gasÓ¦fI^L- (€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.1‹KL1œ’’’’’’’’7’’’’L €ė±^LzM: 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„M( €€˜˜‚Q€ ‚’ ĢzM°O? 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!„M €) "€B€†Ų”Q€‚’Specific heat is not constant.°O €^L1°O=€1x’’’’’’’’8’’’’=€„†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€ ‚’7ś(Šƒ= 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.%ėSƅ: 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§Šƒ„†. *€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.1ƅµ†1Ö’’’’’’’’9’’’’µ†Zˆė±„† ‡: 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+µ†Ė‡( €€˜˜‚Q€ ‚’a ‡Zˆ. ,€Ā€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1Ė‡‹ˆ1ļ’’’’’’’’:’’’’‹ˆI‹ė±Zˆv‰: 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+‹ˆ”‰( €€˜˜‚Q€ ‚’Økv‰I‹= 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”‰z‹1’’’’’’’’;’’’’z‹ZĄė±I‹eŒ: 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‹Œ( €€˜˜‚Q€ ‚’ßeŒƎ@ 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.ŸjŒZĄ5 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 wƎZĄI‹ith Steps 1 through 6, click on the Exit button to go back tothe Main menu.1Ǝ‹Ą1ī’’’’’’’’<’’’’‹ĄHĆė±ZĄvĮ: 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+‹Ą”Į( €€˜˜‚Q€ ‚’§jvĮHĆ= 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”ĮyĆ1’’’’’’’’=’’’’yĆLČė±HĆdÄ: 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+yƏÄ( €€˜˜‚Q€ ‚’ŽdÄ­Ę@ 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ÄLČ5 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.1­Ę}Č1“’’’’’’’’>’’’’}Čߏė±LČhÉ: 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+}Č“É( €€˜˜‚Q€ ‚’LhÉߏ; 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“ÉĖ1’’’’’’’’?’’’’ĖnĻė±ßŹūĖ: 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+Ė&Ģ( €€˜˜‚Q€ ‚’3šūĖYĪC 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 defaultć&ĢnĻ2 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.1YĪŸĻ1”’’’’’’’’@’’’’ŸĻĒė±nĻ–: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180,ŸĻ–nĻ Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŸĻĮ( €€˜˜‚Q€ ‚’Ė–Ē; 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 losses1Įų1Ü’’’’’’’’A’’’’ų£ė±Ēć: 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+ų( €€˜˜‚Q€ ‚’ßć,? 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.=i< 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:,£) "€"€†Ų”Q€‚’the Main menu.1iŌ1 ’’’’’’’’B’’’’Ō­ ė±£æ : 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+Ōź ( €€˜˜‚Q€ ‚’Ć‰æ ­ : 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 losses1ź Ž 1)’’’’’’’’C’’’’Ž Aė±­ 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+Ž ō ( €€˜˜‚Q€ ‚’ŌÉ > 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 theĘō A: 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 valuA­ es 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.1CA1Ą’’’’’’’’D’’’’CAŅBė±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+CAYB( €€˜˜‚Q€ ‚’yK.BŅB. ,€–€†Ų”Q€‚€‚‚’Compressible FlowThis section provides analysis of compressible flow.1YBC1R’’’’’’’’E’’’’C$Eė±ŅBīC: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+CD( €€˜˜‚Q€ ‚’ ÓīC$E8 >€§€†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 constant1DUE15’’’’’’’’F’’’’UEYHė±$E@F: 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+UEkF( €€˜˜‚Q€ ‚’ī²@FYH< 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.1kFŠH1M’’’’’’’’G’’’’ŠH¦Jė±YHuI: 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+ŠH I( €€˜˜‚Q€ ‚’ĪuI¦J8 >€€†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 I×J1¦’’’’’’’’H’’’’×JLNė±¦JĀK: 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€ ‚’%ēĀKN> 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:ķKLN) "€"€†Ų”Q€‚’the Main menu.1N}N1 ’’’’’’’’I’’’’}NZ€ė±LNhO: 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+}N“O( €€˜˜‚Q€ ‚’»‹hOZ€0 .€€†Ų”Q€‚€‚‚‚’Compressible Flow: PropertiesThis subsection provides an“OZ€LNalysis od stagnation and static properties inthe case of compressible flow.1“O‹€1Š’’’’’’’’J’’’’‹€ä‚ė±Z€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+‹€”( €€˜˜‚Q€ ‚’C vä‚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”ƒ1I’’’’’’’’K’’’’ƒ-‡ė±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+ƒ+„( €€˜˜‚Q€ ‚’*ź„U†@ 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 stagnationŲŖ+„-‡. *€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.1U†^‡1~’’’’’’’’L’’’’^‡«‰ė±-‡Iˆ: 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+^‡tˆ( €€˜˜‚Q€ ‚’7’Iˆ«‰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 constant1tˆ܉1K’’’’’’’’M’’’’܉öė±«‰ĒŠ: 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+܉ņŠ( €€˜˜‚Q€ ‚’0ņĒŠ"> 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¦ņŠö. *€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.1"'Ž1Ö’’’’’’’’N’’’’'ŽŠĄė±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+'Ž=( €€˜˜‚Q€ ‚’A ŠĄ8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: NozzleThis subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation=ŠĄö Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1=»Ą1T’’’’’’’’O’’’’»ĄŽÄė±ŠĄ¦Į: 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+»ĄŃĮ( €€˜˜‚Q€ ‚’)ė¦ĮśĆ> 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,äµŃĮŽÄ/ ,€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.1śĆÅ1M’’’’’’’’P’’’’Å+Čė±ŽÄśÅ: 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+Å%Ę( €€˜˜‚Q€ ‚’ŹśÅ+Č< 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 constant1%Ę\Č1į’’’’’’’’Q’’’’\Č Ķė±+ČGÉ: 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+\ČrÉ( €€˜˜‚Q€ ‚’ ĢGÉ|Ė> 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_rÉ Ķ1 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|Ė=Ķ1Œ’’’’’’’’R’’’’=Ķ˜Ļė± 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+=ĶSĪ( €€˜˜‚Q€ ‚’E (Ī˜Ļ8 >€€†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 constant1SĪÉĻ1Ź’’’’’’’’S’’’’ÉĻźė±˜ĻĄ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ÉĻĄ˜Ļƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ÉĻė( €€˜˜‚Q€ ‚’ŻĄ> 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,äµėź/ ,€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.11Į’’’’’’’’T’’’’«ė±ź: 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+1( €€˜˜‚Q€ ‚’zA«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 constant11Ü1’’’’’’’’U’’’’ÜĒ ė±«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+Üņ( €€˜˜‚Q€ ‚’.šĒ > 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§pņĒ 7 <€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.1 ų 1]’’’’’’’’V’’’’ų $ ,Ē $ ) "€€†Ų”Q€‚’1ų ’’’’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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