?_u’’’’³‹e\lŁ„J[+’’’•ĒB«’’’’śĒBin-#dctlg [+oM[+’’š™ĒBę’’’’>ŒĒBin ware€†Ų”Q’’’’’’’’'’’’’’’’’’’--#j [+rM[+’’‚˜ĒB‡’’’’nĒB  ’’Ą€†Ų”Qial b [+jI[+’’†“ĒBÉ’’’’ü’ĒB-#Couri[+qQ[+’’3mR -#UCog [+oI[+’’l™ĒBÉ’’’’*“ĒBCY iU€†Ų”QCYR BaljUCourier New TU-#kU[+ F[+’’–ĒB’’’’Ŗ‘ĒBw -#em  [+ØI[+’’†˜ĒB2ÆD¦D’’’’ 1’’’’=1Ó’’’’’’’’=oé° &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.comI$=o% €H€°°€‚’Power Systems Analysis 1.1 - HelpØS&U z€¦€˜˜ć\ŖÓP€‰€‚ćS?€‰€‚ć$ēdI€‰€‚怉€‚’Program DescriptionClaim SheetHow to Use the ProgramProperties¤Qo»S v€¢€˜€ƒć> € ‰€ ‚€ƒć? € ‰€ ‚€ƒć@ € ‰€ ‚’Temperature - PressureEnthalpy - PressureEntropy - Pressure@ū. ,€$€°˜ć€‰€‚’Power Cycles^»YB T€8€˜€ƒć°€ ‰€ ‚€ƒć±€ ‰€ ‚’CarnotBrayton½[ūb ”€¶€Œ€ƒƒćn«€ ‰€ ‚€ƒƒćo«€ ‰€ ‚€ ƒƒćp«‰€ ‚€ ƒƒćq«‰€ ‚’Power (Ideal)Power (Real)Propulsion (Ideal)Propulsion (Real)n$Y„J d€H€˜€ ƒć²‰€ ‚€ ƒć³‰€ ‚€ ƒć“‰€ ‚’RankineOttoDieselT&Ų. ,€L€°˜ć€‰€‚’Power Cycle Components/ProcessesD„1 2€&€˜€ƒćé€ ‰€ ‚’CompressionCŲ¬M j€†€Œ€ ƒƒćęB߉€ ‚€ ƒƒćēB߉€ ‚€ ƒƒćčB߉€ ‚’Isentropic (Ideal)Isentropic (Real)Isothermal?ė. ,€"€˜€ ƒćź‰€ ‚’CombustionX¬C> L€4€Œ€ ƒƒćJ߉€ ‚€ ƒƒć J߉€ ‚’Coal/OilGas>ė. ,€ €˜€ ƒćė‰€ ‚’ExpansionCCM j€†€Œ€ ƒƒćXQ߉€ ‚€ ƒƒćYQ߉€ ‚€ ƒƒćZQ߉€ ‚’Isentropic (Ideal)Isentropic (Real)Isothermal1B1€ ’’’’’’’’’’’’B@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+BV( €€˜˜‚Q€ ‚’6ś+Œ < F€õ€€‚€ ‚€ € ‚€ € ‚‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power Systems Analysis, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, analyzes power cycles and power cycle components/processes.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofpower systems. It should provide you with the opportunity to moreĻVœ A P€Ÿ€€ ‚‚‚‚‚€ € € € ‚‚€ ‚€ ƒ‚ƒ‚’quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outmore about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (301) 540-3605.Thermodynamic and Transport PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureŖUŒ FU x€«€€ ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚’Entropy and PressurePower CyclesCarnotBrayton (Power and Propulsion)RankineOttoDieselPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:j:œ °0 0€t€‘€†üE”€ ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ßF», &€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 Softw»@areP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1»Ī@1o’’’’’’’’’’’’Ī@ H鰝@·A9 @€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+Ī@āA( €€˜˜‚Q€ ‚’ Ė·AėC> 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:"ąāA FB 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’·ėC HH ^€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 F=H1?’’’’’’’’’’’’=HKKé° H&I9 @€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+=HQI( €€˜˜‚Q€ ‚’śæ&IKK; D€€†Ų”Q€‚€ ‚€ € ‚‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Power Systems Analysis program,the user needs to change one or more input values in order to calculatea new case. Input values are in boxes with white background and canbe changed by clicking on each individual box or even by using thearrow keys and changing the current value. Output values cannot bemodified, changed by the user and they are in boxes with blackbackground.1QI|K1±’’’’’’’’’’’’|KüNé°KKeL9 @€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+|KL( €€˜˜‚Q€ ‚’ßeL„N6 :€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.LüN) "€\€†Ų”Q€ ‚’steam table calculations are not available.1„N-O1Ž’’’’’’’’’’’’-O–é°üN"€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://ww-O"€üNw.engineering-4e.com+-OM€( €€˜˜‚Q€ ‚’I"€–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 constant1M€Ē1£’’’’’’’’’’’’Ē9…ķ±–“‚< F€c€†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+Ēß‚( €€˜˜‚Q€ ‚’ ā“‚’„> 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:߂9…) "€"€†Ų”Q€ ‚’the Main menu.1’„j…1…’’’’’’’’’’’’j…¾‡é°9…S†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+j…~†( €€˜˜‚Q€ ‚’@S†¾‡9 @€€†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 constant1~†ļ‡1•’’’’’’’’’’’’ļ‡S‹é°¾‡Ųˆ9 @€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+ļ‡‰( €€˜˜‚Q€ ‚’ŁŲˆ‹= 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:‰S‹) "€"€†Ų”Q€ ‚’the Main menu.1‹„‹1€’’’’’’’’ ’’’’„‹Óé°S‹mŒ9 @€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+„‹˜Œ( €€˜˜‚Q€ ‚’;mŒÓ8 >€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚’Properties: Entropy - PressureThis subsection provides physical properties of the selected specie forassigned entropy and pressure.Input Values:Specie, Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1˜ŒŽ1’’’’’’’’’ ’’’’ŽqĮé°ÓķŽ9 @€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+Ž( €€˜˜‚Q€ ‚’ÖķŽ7Į= 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 defau7ĮӍlt 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:qĮ) "€"€†Ų”Q€ ‚’the Main menu.17Į¢Į1 ’’’’’’’’ ’’’’¢Į~Åé°qĮ‹Ā9 @€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+¢Į¶Ā( €€˜˜‚Q€ ‚’(ķ‹ĀŽÄ; D€Ū€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚’CoefficientsFor each reaction specie, the thermodynamic functions specific heat,enthalpy and entropy as functions of temperature are given in the form ofleast squares coefficients as follows:Cp/R = A1 + A2*T + A3*T^2 + A4*T^3 + A5*T^4 [/]H/(R*T) = A1 + A2*T/2 + A3*T^2/3 + A4*T^3/4 + A5*T^4/5 + A6/T [/]S/R = A1*lnT + A2*T + A3*T^2/2 + A4*T^3/3 + A5*T^4/4 + A7 [/]For each specie, two sets of coefficients are included for two adjecent v¶Ā~Å* $€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.1ŽÄÆÅ1©’’’’’’’’ ’’’’ÆÅ'Čé°~ŘĘ9 @€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+ÆÅĆĘ( €€˜˜‚Q€ ‚’d,˜Ę'Č8 >€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.1ĆĘXČ1 ’’’’’’’’ ’’’’XČ4Źé°'ČAÉ9 @€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+XČlÉ( €€˜˜‚Q€ ‚’ȘAÉ4Ź0 .€1€†Ų”Q€‚€ ‚‚‚’Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1lÉeŹ1’’’’’’’’’’’’eŹ4Ķé°4ŹNĖ9 @€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+eŹyĖ( €€˜˜‚Q€ ‚’»ƒNĖ4Ķ8 >€€†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 Properties1yĖeĶ1Ś’’’’’’’’’’’’eĶČé°4ĶNĪ9 @€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+eĶyĪ( €€˜˜‚Q€ ‚’ ĢNĪŽ= 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 thyĪŽ4Ķe steam propertiesfor the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back to:yĪČ) "€"€†Ų”Q€ ‚’the Main menu.1Žł1U’’’’’’’’’’’’łé°Čā9 @€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+ł ( €€˜˜‚Q€ ‚’Ņā> 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.1 N1§’’’’’’’’’’’’NÄé°79 @€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+Nb( €€˜˜‚Q€ ‚’b,7Ä6 :€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 Properties1bõ1W’’’’’’’’’’’’õ é°ÄŽ9 @€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+õ ( €€˜˜‚Q€ ‚’ÕŽ = 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.1 L 1ē’’’’’’’’’’’’L  é° 5 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+L ` ( €€˜˜‚Q€ ‚’¢s5  / .€ę€†Ų”Q€‚€ ‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto and Diesel).1` 3 1Ģ’’’’’’’’’’’’3 Īé°  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+3 G ( €€˜˜‚Q€ ‚’‡N Ī9 @€€†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.1G ’1V’’’’’’’’’’’’’@Bé°Ī @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’ @Ī+’7@( €€˜˜‚Q€ ‚’ Ģ @@B= H€™€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: CarnotSTEP 1Enter the desired heat addition temperature value or go with the defaulttemperature value.STEP 2Enter the desired heat rejection temperature value or go with the defaulttemperature value.STEP 3Click on the Calculate button to start the calculation of the Carnot cycleoutput values for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.17@qB1ž’’’’’’’’’’’’qB>Dé°@BZC9 @€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+qB…C( €€˜˜‚Q€ ‚’¹‰ZC>D0 .€€†Ų”Q€‚€ ‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1…CoD1’’’’’’’’’’’’oDBHé°>DXE9 @€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+oDƒE( €€˜˜‚Q€ ‚’ŪXE™G; 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.©ƒEBH* $€ž€†Ų”Q€ ‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1™GsH1i’’’’’’’’’’’’sH«Mé°BH\I9 @€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+sH‡I( €€˜˜‚Q€ ‚’@\IĒK? 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䫇I«M9 @€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.1ĒKÜM1’’’’’’’’’’’’ÜM‚é°«MÅN9 @€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+ÜMšN( €€˜˜‚Q€ ‚’ŪÅN9 @€·€†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 InletTempšN«Merature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateÕšN‚. *€«€†Ų”Q€ ‚‚‚‚‚’Assumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1D‚1ī’’’’’’’’’’’’D‚‰é°‚-ƒ9 @€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+D‚Xƒ( €€˜˜‚Q€ ‚’?-ƒ—…? 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 defaultAXƒŲ‡< F€ €†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 8Enter the compressor isentropic efficiency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor)÷—…‰2 2€ļ€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’efficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go back to the Main menu.1Ų‡2‰1’’’’’’’’’’’’2‰é°‰Š9 @€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+2‰FŠ( €€˜˜‚Q€ ‚’9żŠŒ< 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›qFŠ* $€ā€†Ų”Q€ ‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ŒK1Ź’’’’’’’’’’’’K”Ā鰍4Ž9 @€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+K_Ž( €€˜˜‚Q€ ‚’E4Ž°Ą? 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 t_Ž°Ąhe desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultä«_Ž”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°ĄÅĀ1o’’’’’’’’’’’’ÅĀĒ鰔Ā®Ć9 @€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+ÅĀŁĆ( €€˜˜‚Q€ ‚’I ®Ć"Ę< F€€†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 HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.į¶ŁĆĒ+ $€m€†Ų”Q€ ‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1"Ę4Ē1š’’’’’’’’’’’’4ĒóĶé°ĒČ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+4ĒHČ( €€˜˜‚Q€ ‚’DČŒŹ? L€ €†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultAHČĶĢ< F€ €†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the compressor isentropic efficiency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor&õŒŹóĶ1 0€ė€†Ų”Q€ ‚‚‚‚‚‚‚‚’efficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1ĶĢ$Ī1_’’’’’’’’’’’’$ĪŁé°óĶ Ļ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+$Ī8Ļ( €€˜˜‚Q€ ‚’•[ ĻŁ: B€·€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: RankineThis subsection provides analysis of the Rankine cycle.Input Values:Turbine Inlet Conditions (Temperature and Pre8ĻŁóĶssure), Steam Mass FlowRate, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion and heattransfer.18Ļ 1ā’’’’’’’’ ’’’’ »é°Łó9 @€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+ ( €€˜˜‚Q€ ‚’Óó-< 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.Žb», (€Ä€†Ų”Q€ ‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1-ģ1Ł’’’’’’’’!’’’’ģ”é°»Õ9 @€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+ģ( €€˜˜‚Q€‚’*ńÕ*9 @€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 Revolutions, Fuel HHVNumber of Cylinders, Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel Consumptionj?”+ &€~€†Ų”Q€ ‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1*Å1µ’’’’’’’’"’’’’ÅI鰔® 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+ÅŁ ( €€˜˜‚Q€ ‚’)ź®  ? 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!åŁ #< F€Ė€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’temperature value.STEP 6Enter the desired number of revolutions value or go with the defaultnumber of revolutions value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the desired number of cylinders value or go with the default numberof cylinders value.STEP 9Enter the desired cylinder stroke value or go with the default cylinderstroke value.STEP 10Enter the desired stroke to diameter value or go with the default stroke&ō I2 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#z1"’’’’’’’’#’’’’zDCé°Io@9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-zo@I3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+zš@( €€˜˜‚Q€ ‚’2ło@ĢB9 @€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 Revolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelxLš@DC, (€˜€†Ų”Q€ ‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1ĢBuC1Ė’’’’’’’’$’’’’uCJé°DC^D9 @€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+uC‰D( €€˜˜‚Q€ ‚’/š^DøF? L€į€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: DieselSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired cut-off ratio (volumetric) value or go with the default,š‰DäH< F€į€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’cut-off ratio value.STEP 6Enter the desired number of revolutions value or go with the defaultnumber of revolutions value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the desired number of cylinders value or go with the default numberof cylinders value.STEP 9Enter the desired cylinder stroke value or go with the default cylinderstroke value.STEP 10Enter the desired stroke to diameter ratio value or go with the default stroke to+łøFJ2 2€ó€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’diameter ratio value.STEP 11Click on the Calculate button to start the calculation of the Diesel cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1äH@J1“’’’’’’’’%’’’’@J¢Né°J)K9 @€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+@JTK( €€˜˜‚Q€ ‚’2ł)K†M9 @€ó€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: MagnetohydrodynamicsThis subsection provides analysis of the Magnetohydrodynamics cycle.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet Stagnation Pressure,Velocity, Conductivity, Loading Parameter, Magnetic Field Strength,Channel Length, MobilityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Hall Voltage, Outlet StaticTemperature, Outlet Static Pressure, Outlet Mach Number, OutletķTK¢N/ ,€Ū€†Ų”Q€ ‚‚‚‚‚‚’Stagnation Temperature, Outlet Stagnation Pressure, Specific WorkOutput, Enthalpy ExtractionAssumptions:Specific heat, velocity, conductivity, mobility, induced voltage field, Hallvoltage and magnetic field strength are constant.1†MÓN1<’’’’’’’’&’’’’ÓN…é°¢N¼O9 @€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+ÓN €( €€˜˜‚Q€ ‚’¼O €¢N4ö¼O@‚> 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  €ˆ„< 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@‚…, (€Č€†Ų”Q€ ‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1ˆ„I…1Ą’’’’’’’’'’’’’I…Ų‡é°…2†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+I…]†( €€˜˜‚Q€ ‚’ß2†k‡/ ,€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:mD]†Ų‡) "€ˆ€†Ų”Q€ ‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1k‡ ˆ1’’’’’’’’(’’’’ ˆeŒé°Ų‡ņˆ9 @€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+ ˆ‰( €€˜˜‚Q€ ‚’ įņˆ=‹? 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(ö‰eŒ2 2€ķ€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’temperature value.STEP 6Click on the Calculate button to start the calculation of the Fuel Cell cycleoutput values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1=‹–Œ1’’’’’’’’)’’’’–ŒkŽé°eŒ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+–ŒŖ( €€˜˜‚Q€ ‚’Į‘kŽ0 .€#€†Ų”Q€‚€ ‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1ŖœŽ1Ų’’’’’’’’*’’’’œŽOĄé°kŽ…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+œŽ°( €€˜˜‚Q€ ‚’“e…OĄ. ,€Ź€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes:°OĄkŽ CompressionThis subsection provides analysis of compression.1°€Ą1ņ’’’’’’’’+’’’’€ĄAĆé°OĄiĮ9 @€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+€Ą”Į( €€˜˜‚Q€ ‚’­piĮAĆ= 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”ĮrĆ1Ö’’’’’’’’,’’’’rĆČé°AĆ[Ä9 @€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+rƆÄ( €€˜˜‚Q€ ‚’ Ē[ďĘB 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 5ˆU†ÄČ3 4€«€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1ĘHČ1’’’’’’’’-’’’’HČ+Ėé°Č1É9 @€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+HČ\É( €€˜˜‚Q€ ‚’Ļ‘1É+Ė> J€#€†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 Pressure, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1\É\Ė1’’’’’’’’.’’’’\ĖŽé°+ĖEĢ9 @€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+\ĖpĢ( €€˜˜‚Q€ ‚’ĘEĢxĪB 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 5 ŌpĢŽ6 :€©€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Enter the desired compressor isentropic efficiency value or go with thedefault compressor isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of compressor outlettemperature and power input vaxĪŽ+Ėlues for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1xĪæ1Õ’’’’’’’’/’’’’æc鰎Ø9 @€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+æÓ( €€˜˜‚Q€ ‚’SØc= 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 compression1Ó”1ž’’’’’’’’0’’’’”é°c}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+”Ø( €€˜˜‚Q€ ‚’Až}éC 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 defaultęØ2 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.1é21Ö’’’’’’’’1’’’’2× 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+2F ( €€˜˜‚Q€ ‚’‘c × . ,€Ę€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1F  1§’’’’’’’’2’’’’ ~ é°× ń 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+  ( €€˜˜‚Q€ ‚’Łń 4 ? 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! ~ ) "€B€†Ų”Q€ ‚’Specific heat is not constant.14 Æ 1;’’’’’’’’3’’’’Æ  Dé°~ ˜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+Æ Ć( €€˜˜‚Q€ ‚’B˜A< 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 noĆA~ rmalize 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.%ėĆ6C: 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¦A D- (€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.16C:D1š’’’’’’’’4’’’’:D£Gé° D#E9 @€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+:DNE( €€˜˜‚Q€ ‚’ Ģ#EYG? 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!NE£G) "€B€†Ų”Q€ ‚’Specific heat is not constant.1YGŌG1v’’’’’’’’5’’’’ŌGNé°£G½H9 @€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+ŌGčH( €€˜˜‚Q€ ‚’7ś½HK= 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.%ėčHDM: 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§KN. *€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.1DMJN1Ō’’’’’’’’6’’’’JN €é°N3O9 @€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+JN^O( €€˜˜‚Q€ ‚’a3O €. ,€Ā€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.^O €N1^O=€1ķ’’’’’’’’7’’’’=€ł‚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+=€Q( €€˜˜‚Q€ ‚’Øk&ł‚= 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.1Q*ƒ1’’’’’’’’8’’’’*ƒü‡é°ł‚„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+*ƒ>„( €€˜˜‚Q€ ‚’ß„]†@ 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>„ü‡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.1]†-ˆ1 ’’’’’’’’9’’’’-ˆ‹é°ü‡‰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+-ˆA‰( €€˜˜‚Q€ ‚’ň‰‹= H€€†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 Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1A‰7‹1’’’’’’’’:’’’’7‹ĶĄé°‹ Œ9 @€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‹KŒ( €€˜˜‚Q€ ‚’Ž ŒiŽ@ 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. čKŒ•Ą8 >€Ń€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter the desired turbine/expander mass flow rate value or go with thedefault mass flow rate value.STEP 6Enter the desired turbine/expander isentropic efficiency value or go with the default turbine/expander isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of turbine/expanderoutlet temperaturiŽ•Ą‹e and power output values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back to8iŽĶĄ( € €†Ų”Q€ ’the Main menu.1•ĄžĄ1‘’’’’’’’’;’’’’žĄ^Ćé°ĶĄēĮ9 @€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+žĄĀ( €€˜˜‚Q€ ‚’LēĮ^Ć; 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 expansion1ĀĆ1’’’’’’’’<’’’’ĆėĒé°^ĆxÄ9 @€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+Ć£Ä( €€˜˜‚Q€ ‚’3šxÄÖĘC 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£ÄėĒ2 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.1ÖĘČ1K’’’’’’’’=’’’’Č6Ėé°ėĒÉ9 @€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+Č0É( €€˜˜‚Q€ ‚’ĖÉ6Ė; 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 losses10ÉgĖ1m’’’’’’’’>’’’’gĖé°6ĖPĢ9 @€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+gĖ{Ģ( €€˜˜‚Q€ ‚’ßPĢ™Ī? 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.={Ģā< 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 temperatur™Īā6Ėe 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:™Ī) "€"€†Ų”Q€ ‚’the Main menu.1āM1’’’’’’’’?’’’’M$é°69 @€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+Ma( €€˜˜‚Q€ ‚’Ɖ6$: B€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: MixingThis subsection provides analysis of mixing.Input Values:Inlet Working Fluids (Species), Inlet Working Fluids Mass Flow Rate, InletWorking Fluids Temperature, Outlet Working Fluids (Species), Outlet WorkingFluids Mass Flow RateOutput Values:Outlet Working Fluids Temperature -- Mixing TemperatureAssumptions:Ideal mixing -- no losses1aU1W’’’’’’’’@’’’’U{ é°$>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+Ui( €€˜˜‚Q€ ‚’Ō>{> 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 theĘi{ : B€€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’default temperature value.STEP 5Select the desired outlet species (outlet working fluid) or go with the defaultspecies.STEP 6Enter the desired outlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 7Click on the Calculate button to start the calculation of mixing outletvalues for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1{¬ 1¾’’’’’’’’A’’’’¬ 9 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+¬ Ą ( €€˜˜‚Q€ ‚’yK• 9 . ,€–€†Ų”Q€‚€ ‚‚’Compressible FlowThis section provides analysis of compressible flow.1Ą j 1P’’’’’’’’B’’’’j ‰ é°9 S 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+j ~ ( €€˜˜‚Q€ ‚’ ÓS ‰ 8 >€§€†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 constant1~ ŗ 1¬’’’’’’’’C’’’’ŗ Č@鰉 £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+ŗ Ī( €€˜˜‚Q€ ‚’ī²£Č@< 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 CalculaĪČ@‰ te 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.1Īł@1K’’’’’’’’D’’’’ł@Cé°Č@āA9 @€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+ł@ B( €€˜˜‚Q€ ‚’ĪāAC8 >€€†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 BDC1¤’’’’’’’’E’’’’DC·Fé°C-D9 @€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+DCXD( €€˜˜‚Q€ ‚’%ē-D}F> 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:XD·F) "€"€†Ų”Q€ ‚’the Main menu.1}FčF1’’’’’’’’F’’’’čF·Hé°·FŃG9 @€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+čFüG( €€˜˜‚Q€ ‚’»‹ŃG·H0 .€€†Ų”Q€‚€ ‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1üGčH1ˆ’’’’’’’’G’’’’čH?Ké°·HŃI9 @€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+čHüI( €€˜˜‚Q€ ‚’C ŃI?K8 >€€†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 constant1üIpK1G’’’’’’’’H’’’’pK†Oé°?KYL9 @€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+pK„L( €€˜˜‚Q€ ‚’*źYL®N@ 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„L†O. *€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®N·O1ģ’’’’’’’’I’’’’·O‚鰆O¬€9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering Sof·O¬€†OtwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+·O׀( €€˜˜‚Q€ ‚’7’¬€‚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 constant1׀?‚1I’’’’’’’’J’’’’?‚W†é°‚(ƒ9 @€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+?‚Sƒ( €€˜˜‚Q€ ‚’0ņ(ƒƒ…> 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¦SƒW†. *€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.1ƒ…ˆ†1†’’’’’’’’K’’’’ˆ†Żˆé°W†q‡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+ˆ†œ‡( €€˜˜‚Q€ ‚’A q‡Żˆ8 >€€†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 constant1œ‡‰1R’’’’’’’’L’’’’‰/é°Żˆ÷‰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+‰"Š( €€˜˜‚Q€ ‚’)ė÷‰KŒ> 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,äµ"Š// ,€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.1KŒ`1•’’’’’’’’M’’’’`†Ąé°/IŽ9 @€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+`tŽ( €€˜˜‚Q€ ‚’ŹIŽ†Ą< 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, OutlettŽ†Ą/Velocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1tŽ·Ą1ß’’’’’’’’N’’’’·ĄeÅ鰆Ą Į9 @€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+·ĄĖĮ( €€˜˜‚Q€ ‚’ Ģ ĮÕĆ> 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_ĖĮeÅ1 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.1ÕĆ–Å1Š’’’’’’’’O’’’’–ÅļĒé°eÅĘ9 @€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+–ÅŖĘ( €€˜˜‚Q€ ‚’E ĘļĒ8 >€€†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 constant1ŖĘ Č1D’’’’’’’’P’’’’ Č3Ģé°ļĒ É9 @€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+ Č4É( €€˜˜‚Q€ ‚’Ż ÉOĖ> 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,äµ4É3Ģ/ ,€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.1OĖdĢ1æ’’’’’’’’Q’’’’dĢņĪé°3ĢMĶ9 @€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+dĢxĶ( €€˜˜‚Q€ ‚’zAMĶņĪ9 @€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 constant1xĶ#Ļ1’’’’’’’’R’’’’#Ļé°ņĪ9 @€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.engineer#ĻņĪing-4e.com+#ĻC( €€˜˜‚Q€ ‚’.šq> 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§pC7 <€į€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚’rate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 8When done with Steps 1 through 7, click 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