?_p’’’’é”`Wlˆ ĪMEnergy Conversion ... - HelpEngineering Software (c) 1996/&;)z4˜^‹F Ęué’’Æ’’’’|CONTEXTŗŒ|CTXOMAP€„|FONT}O|SYSTEM|TOPICŸ|TTLBTREE‹„ĒB³’’’’&hĒBGu-#he¤[+¬F[+’’mĒBō’’’’ÖgĒBV-#‚[+ŠO[+’’ pĒB’’’’ŹeĒB %[+’’’’-#:} [+…J[+’’jmĒB˜’’’’öhĒBœo fE€†Ų”Q’’’’»-#®mĒBr[+zE[+’’²kĒB*’’’’VkĒB-#ingLw[+E[+’’ĪpĒB*’’’’„kĒB Myri€˜˜‚Qd WeĮbMyriad Web-#Albe¾ [+ĘL[+’’\nĒB’’’’ÖiĒB-#5.[+#O[+’’ŲlĒB9’’’’ŗgĒBrd-#dctlå[+ķR[+’’qĒBV’’’’°hĒBin1Software%okma’’’’’’’’’’’’’’’’’’’’ Ź_G-#U[+]O[+’’mĒB:’’’’…>l-##¬[+“H[+’’œmĒBõ’’’’ČjĒBŲl_nowidctlparcs16Osuper#Engineering Softwarer-#†ŲØ [+°J[+’’‚pĒB™’’’’0kĒBHet-#rrow¶ [+¾J[+’’ŹmĒBö’’’’ÕmĒB-#’’Ź [+ŅJ[+’’8nĒBö’’-#œmĒB‚ [+ŠL[+’’&pĒBE’’’’2hĒB-#ŽpĒB[+%R[+’’šwĒBc’’’’&fĒB-#rpĒBh[+pD[+’’ÄsĒŽJÕJ’’’’ 1’’’’=1 ’’’’’’’’=j> 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.comD=j% €>€°°€‚’Energy Conversion 1.1 - HelpØS&U z€¦€˜˜ć\ŖÓP€‰€‚ćS?€‰€‚ć$ēdI€‰€‚怉€‚’Program DescriptionClaim SheetHow to Use the ProgramPropertiesČdjŚd ˜€Č€˜€ƒć> € ‰€ ‚€ƒć? € ‰€ ‚€ƒć@ € ‰€ ‚€ƒćA € ‰€ ‚’Temperature - PressureEnthalpy - PressureEntropy - PressureCoefficientsH". ,€4€°˜ć€‰€‚’Steam Approximationso-Ś‘B T€Z€˜€ƒćw€ ‰€ ‚€ƒćx€ ‰€ ‚’Saturated AreaSuperheated Area@"Ń. ,€$€°˜ć€‰€‚’Power Cycles^‘/B T€8€˜€ƒć°€ ‰€ ‚€ƒć±€ ‰€ ‚’CarnotBrayton½[Ńģb ”€¶€Œ€ƒƒćn«€ ‰€ ‚€ƒƒćo«€ ‰€ ‚€ ƒƒćp«‰€ ‚€ ƒƒćq«‰€ ‚’Power (Ideal)Power (Real)Propulsion (Ideal)Propulsion (Real)³M/Ÿf œ€š€˜€ ƒć²‰€ ‚€ ƒć³‰€ ‚€ ƒć“‰€ ‚€ ƒćµ‰€ ‚€ ƒć¶‰€ ‚’RankineOttoDieselMagnetohydrodynamicsFuel CellT&ģó. ,€L€°˜ć€‰€‚’Power Cycle Components/ProcessesDŸ71 2€&€˜€ƒćé€ ‰€ ‚’CompressionCóĒM j€†€Œ€ ƒƒćęB߉€ ‚€ ƒƒćēB߉€ ‚€ ƒƒćčB߉€ ‚’Isentropic (Ideal)Isentropic (Real)Isothermal?7. ,€"€˜€ ƒćź‰€ ‚’CombustionXĒ^> L€4€Œ€ ƒƒćJ߉€ ‚€ ƒƒć J߉€ ‚’Coal/OilGas>œ. ,€ €˜€ ƒćė‰€ ‚’ExpansionC^,M j€†€Œ€ ƒƒćXQ߉€ ‚€ ƒƒćYQ߉€ ‚€ ƒƒćZQ߉€ ‚’Isentropic (Ideal)Isentropic (Real)Isothermal\ œˆ< H€@€˜€ ƒćģ‰€ ‚€ ƒćķ‰€ ‚’Heat TransferMixingE,Ķ. ,€.€°˜ć€‰€‚’Compressible Flowƒ9ˆP J d€r€˜€ ƒć"&‰€ ‚€ ƒć#&‰€ ‚€ ƒć$&‰€ ‚’Velocity of SoundMach NumberProperties]Ķ­ > L€>€Œ€ ƒƒć |‰€ ‚€ ƒƒć |‰€ ‚’StagnationStatic‘9P > X €€r€˜€ ƒć%&‰€ ‚€ ƒć&&‰€ ‚€ ƒć'&‰€ ‚€ ƒć(&‰€ ‚’NozzleNormal ShockDiffuserThrust1­ o 1? ’’’’’’’’’’’’o ‰Fé°> X 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+o ƒ ( €€˜˜‚Q€ ‚’8żX » ; D€ū€€‚€ ‚€ € ‚€ € ‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Energy Conversion, that quickly and reliably calculatesthermodynamic and transport properties of gaseous, liquid and solidspecies, contains coefficients for the calculation of the physicalproperties of various species -- the user has the capability to use thecoefficients to carry out independent engineering calculations involvingphysical properties of various species, steam approximations, analyzesģƒ Ņ+ $€Ł€€ ‚‚‚‚‚‚‚‚’power cycles, power cycle components/processes and compressible flow.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunityto more quickly and effectively do your work, explore more options, savetime and give more confidence in carrying out your calculations.To get a free evaluation copy of the program, place an order, find outĄ» ÷AY €€€€ ‚€ € € € Ņ÷A> ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚’more about how you can profit or benefit from this software package,please send an e-mail to info@engineering-4e.com or call (301) 540-3605.Thermodynamic and Transport PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressureCoefficientsSteam ApproximationsSaturated Area (Temperature and Pressure Dependent)Superheated AreaPower CyclesCarnotBrayton (Power and Propulsion) §ŅDc ”€O€€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚’RankineOttoDieselMagnetohydrodynamicsFuel CellPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionHeat TransferMixingCompressible FlowVelocity of SoundMach NumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard drive?÷A@D$ €6€€ ƒ‚’IBM compatible systems:h:DØD. ,€t€†üE”€ ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ß@D³E, &€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„ØD‰F1 0€K€€ ‚€ ‚€ ‚‚‚‚‚‚’Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1³EŗF1o’’’’’’’’’’’’ŗFųM鰉F£G9 @€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+ŗFĪG( €€˜˜‚Q€ ‚’ Ė£G×I> 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:"ąĪGłKB 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’·×IųMH ^€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 constant1łK)N19’’’’’’’’’’’’)N=é°ųMO9 @€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+)N=O( €€˜˜‚Q€ ‚’ōŗO=: B€u€†Ų”Q€‚€ ‚€ € ‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Energy Conversion program, theuser needs to change one or more input valu=O=ųMes in order to calculate anew case. Input values are in boxes with white background and can bechanged by clicking on each individual box or even by using the arrowkeys and changing the current value. Output values cannot be modified,changed by the user and they are in boxes with black background.1=On1±’’’’’’’’’’’’nī„é°=W‚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+n‚‚( €€˜˜‚Q€ ‚’ßW‚—„6 :€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.‚‚ī„) "€\€†Ų”Q€ ‚’steam table calculations are not available.1—„…1Ž’’’’’’’’’’’’…|‡é°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+…3†( €€˜˜‚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 constant13†­‡1£’’’’’’’’’’’’­‡‹ķ±|‡šˆ< 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+­‡Åˆ( €€˜˜‚Q€ ‚’ āšˆåŠ> 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:ň‹) "€"€†Ų”Q€ ‚’the Main menu.1åŠP‹1…’’’’’’’’’’’’P‹¤é°‹9Œ9 @€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+P‹dŒ( €€˜˜‚Q€ ‚’@9Œ¤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 constant1dŒÕ1•’’’’’’’’’’’’ՍEĮé°¤¾Ž9 @€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+ՍéŽ( €€˜˜‚Q€ ‚’Ł¾Ž Į= 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 éŽ Į¤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:éŽEĮ) "€"€†Ų”Q€ ‚’the Main menu.1 ĮvĮ1€’’’’’’’’ ’’’’vĮÅĆé°EĮ_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+vĮŠĀ( €€˜˜‚Q€ ‚’;_ĀÅĆ8 >€€†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 constant1ŠĀöĆ1’’’’’’’’’ ’’’’öĆWĒé°ÅĆßÄ9 @€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+öĆ Å( €€˜˜‚Q€ ‚’ÖßÄĒ= 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: ÅWĒ) "€"€†Ų”Q€ ‚’the Main menu.1ĒˆĒ1~’’’’’’’’ ’’’’ˆĒÕĖé°WĒqČ9 @€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+ˆĒœČ( €€˜˜‚Q€ ‚’)ģqČÅŹ= H€Ł€†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 [/]orS/R = A1*lnT + A2*T + A3*T^2/2 + A4*T^3/3 + A5*T^4/4āœČÕĖ. *€Å€†Ų”Q€ ‚‚‚‚‚’ + A7 - lnp [/]For each specie, two sets of coefficients are included for two adjecenttemperature intervals, 273 to 1,000 K and 1,000 to 5,000 K. The data havebeen constrained to be equal at 1,000 K.1ÅŹĢ1©’’’’’’’’ ’’’’Ģ~Īé°ÕĖļĢ9 @€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+ĢĶ( €€˜˜‚Q€ ‚’d,ļĢ~Ī8 >€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.1ĶÆĪ1h’’’’’’’’ ’’’’ÆĪ—é°~Ī˜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+ÆĪĆĻ( €€˜˜‚Q€ ‚’Ș˜Ļ—0 .€1€†Ų”Q€‚€ ‚‚‚’Steam ApproxĆĻ—~ĪimationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1ĆĻČ1’’’’’’’’’’’’Č—鰗±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+ČÜ( €€˜˜‚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 Properties1ÜČ1ˆ’’’’’’’’’’’’Č鰗±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+ČÜ( €€˜˜‚Q€ ‚’ Ģ±å= 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:Ü) "€"€†Ų”Q€ ‚’the Main menu.1åP1U’’’’’’’’’’’’Pt é°99 @€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+Pd( €€˜˜‚Q€ ‚’Ņ9t > 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.1d„ 1§’’’’’’’’’’’’„  é°t Ž 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+„ ¹ ( €€˜˜‚Q€ ‚’b,Ž  6 :€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 Properties1¹ L 1™’’’’’’’’’’’’L ~@é° 59 @€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€ ‚’Õ5~@= 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 chos`~@ en input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1`Æ@1 ’’’’’’’’’’’’Æ@‡Bé°~@˜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+Æ@ĆA( €€˜˜‚Q€ ‚’Ĕ˜A‡B0 .€)€†Ų”Q€‚€ ‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1ĆAøB1Ģ’’’’’’’’’’’’øBSE鰇B”C9 @€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+øBĢC( €€˜˜‚Q€ ‚’‡N”CSE9 @€€†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.1ĢC„E1N’’’’’’’’’’’’„E”Hé°SEmF9 @€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+„E˜F( €€˜˜‚Q€ ‚’ ĢmF”H= 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˜FŅH1ž’’’’’’’’’’’’ŅHŸJé°”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+ŅHęI( €€˜˜‚Q€ ‚’¹‰»IŸJ0 .€€†Ų”Q€‚€ ‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1ęIŠJ1’’’’’’’’’’’’ŠJ£N鰟J¹K9 @€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+ŠJäK( €€˜˜‚Q€ ‚’Ū¹KśM; 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.©äK£N* $€ž€†Ų”Q€ ‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1śMŌN1a’’’’’’’’’’’’ŌN0„é°£N½O9 @€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+ŌN €( €€˜˜‚Q€ ‚’½O €£N@½OL‚? 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 defaultä« €0„9 @€W€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1L‚a„1\’’’’’’’’’’’’a„Œˆé°0„J…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+a„u…( €€˜˜‚Q€ ‚’ŪJ…‰‡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 InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateÕu…Œˆ. *€«€†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‰‡½ˆ1ī’’’’’’’’’’’’½ˆz鰌ˆ¦‰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+½ˆщ( €€˜˜‚Q€ ‚’?¦‰Œ? 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 defaultAщQŽ< 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)÷Œz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.1QŽ«1e’’’’’’’’’’’’«ŸĆé°z Ą9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O.« Ąz Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+«ĖĄ( €€˜˜‚Q€ ‚’9ż ĄĆ< 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›qĖĄŸĆ* $€ā€†Ų”Q€ ‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ĆŠĆ1n’’’’’’’’’’’’ŠĆ É鰟Ć¹Ä9 @€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+ŠĆäÄ( €€˜˜‚Q€ ‚’E¹Ä)Ē? 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«äÄ É9 @€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)Ē>É1o’’’’’’’’’’’’>É|Ķé° É'Ź9 @€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+>ÉRŹ( €€˜˜‚Q€ ‚’I 'Ź›Ģ< 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¶RŹ|Ķ+ $€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›Ģ­Ķ1­’’’’’’’’’’’’­Ķxé°|Ķ–Ī9 @€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+­ĶĮĪ( €€˜˜‚Q€ ‚’D–Ī? 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 tĮĪ|Ķhe 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 defaultAĮĪR< 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&õx1 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.1R©1Ś’’’’’’’’’’’’©Ré°x’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+©½( €€˜˜‚Q€ ‚’•[’R: 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.1½ƒ1ā’’’’’’’’ ’’’’ƒ4 é°Rl9 @€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€ ‚’Ól¦ < 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—4 , (€Ä€†Ų”Q€ ‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1¦ e 1Ł’’’’’’’’!’’’’e  é°4 N 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+e y ( €€˜˜‚Q€‚’*ńN £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?y  + &€~€†Ų”Q€ ‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1£>1·’’’’’’’’"’’’’>ĪEé° 3@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.comWe>3@ b Site:http://www.engineering-4e.com+>^@( €€˜˜‚Q€ ‚’)ź3@‡B? L€Õ€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: OttoSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired combustion temperature value or go with the default!å^@ØD< 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‡BĪE2 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.1ØD’E1ļ’’’’’’’’#’’’’’E½Ié°ĪEčF9 @€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+’EG( €€˜˜‚Q€ ‚’2łčFEI9 @€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, FuelxLG½I, (€˜€†Ų”Q€ ‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1EIīI1#’’’’’’’’$’’’’īI”€é°½I×J9 @€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+īIK( €€˜˜‚Q€ ‚’/š×J1M? 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,šK]O< 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+ł1M”€2 2€ó€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’diameter ratio value.STEP 11Click on the Calculate button to start the calculation of the Diesel cycleoutput]O”€½I 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]Oŀ1c’’’’’’’’%’’’’ŀ÷„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+ŀŁ( €€˜˜‚Q€ ‚’%ģ®žƒ9 @€Ł€†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 LengthOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Outlet Static Temperature,Outlet Static Pressure, Outlet Mach Number, Outlet StagnationłŹŁ÷„/ ,€•€†Ų”Q€ ‚‚‚‚‚‚’Temperature, Outlet Stagnation Pressure, Enthalpy Extraction,Specific Work OutputAssumptions:Specific heat, velocity, conductivity, induced voltage field andmagnetic field strength are constant.1žƒ(…1ü’’’’’’’’&’’’’(…óŠé°÷„†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€ ‚’4ö†pˆ> 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.F <†¶Š< 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 9Click on the Calculate button to start the calculation of the Magnetohydrodynamics cycle output values for the chosen input values.STEP 10When done with Steps 1 through 9, click on the Exit button to go back=pˆóŠ) "€(€†Ų”Q€ ‚’to the Main menu.1¶Š$‹1Ą’’’’’’’’'’’’’$‹³é°óŠ 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+$‹8Œ( €€˜˜‚Q€ ‚’ß ŒF/ ,€æ€€‚€ ‚‚‚‚‚‚‚‚’Power Cycles: Fuel CellThis subsection provides analysis of the Fuel Cell cycle.Input Values:Fuel, Fuel Inlet Temperature, Oxidant (O2) Inlet Temperature,Fuel Flow Rate, Product Outlet TemperatureOutput Values:mD8Œ³) "€ˆ€†Ų”Q€ ‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1Fä1u’’’’’’’’(’’’’äLĀé°³ĶŽ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+äųŽ( €€˜˜‚Q€ ‚’ įĶŽ$Į? 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 defaulttemperatųŽ$Į³ure value.STEP 3Enter the desired oxidant inlet temperature value or go with the defaulttemperature value.STEP 4Enter the desired fuel flow rate or go with the default fuel flow ratevalue.STEP 5Enter the desired product outlet temperature value or go with the default(öųŽLĀ2 2€ķ€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’temperature value.STEP 6Click on the Calculate button to start the calculation of the Fuel Cell cycleoutput values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1$Į}Ā1’’’’’’’’)’’’’}ĀiÄé°LĀfĆ9 @€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+}Ā‘Ć( €€˜˜‚Q€ ‚’ŲØfĆiÄ0 .€Q€†Ų”Q€‚€ ‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1‘ĆšÄ1Ų’’’’’’’’*’’’’šÄAĘé°iăÅ9 @€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+šÄ®Å( €€˜˜‚Q€ ‚’“eƒÅAĘ. ,€Ź€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1®ÅrĘ1ņ’’’’’’’’+’’’’rĘ3Éé°AĘ[Ē9 @€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+rʆĒ( €€˜˜‚Q€ ‚’­p[Ē3É= 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†ĒdÉ1Ö’’’’’’’’,’’’’dÉ Īé°3ÉMŹ9 @€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+dÉxŹ( €€˜˜‚Q€ ‚’ ĒMŹĢB 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 5ˆUxŹ Ī3 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Ģ:Ī1’’’’’’’’-’’’’:Ī)é° Ī#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+:ĪNĻ( €€˜˜‚Q€ ‚’Ļ‘#Ļ)> J€#€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Compression: Isentropic (Real)This subsection provides analysis of isentropNĻ) Īic 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.1NĻZ1W’’’’’’’’.’’’’Z€é°)C9 @€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+Zn( €€˜˜‚Q€ ‚’ĘCvB 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 Ōn€6 :€©€†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 values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1v±1Õ’’’’’’’’/’’’’±U 鰀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+±Å( €€˜˜‚Q€ ‚’SšU = 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 compression1ņ 1ž’’’’’’’’0’’’’† ó é°U o 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€ ‚’Ažo Ū C 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 defaultęš ó 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 done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1Ū $1Ö’’’’’’’’1’’’’$ @é°ó  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+$8( €€˜˜‚Q€ ‚’‘c  @. ,€Ę€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.8 @ó 18=@1Ŗ’’’’’’’’2’’’’=@³Cé° @&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+=@QA( €€˜˜‚Q€ ‚’Ł&AiC? 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!QA³C) "€B€†Ų”Q€ ‚’Specific heat is not constant.1iCäC1’’’’’’’’3’’’’äC2Jé°³CĶD9 @€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+äCųD( €€˜˜‚Q€ ‚’BĶD:G< 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.%ėųD_I: 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¦:G2J- (€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_IcJ1š’’’’’’’’4’’’’cJĢMé°2JLK9 @€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+cJwK( €€˜˜‚Q€ ‚’ ĢLK‚M? 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!wKĢM) "€B€†Ų”Q€ ‚’Specific heat is not constant.1‚MżM1W’’’’’’’’5’’’’żMN„é°ĢMęN9 @€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+żMO( €€˜˜‚Q€ ‚’7śęNT= 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 OTĢMto 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.%ėOyƒ: 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§TN„. *€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.1yƒ„1Ō’’’’’’’’6’’’’„"†é°N„h…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€ ‚’ah…"†. ,€Ā€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1“…S†1ķ’’’’’’’’7’’’’S†‰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+S†g‡( €€˜˜‚Q€ ‚’Øk<‡‰= 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.1g‡@‰1’’’’’’’’8’’’’@‰Žé°‰)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+@‰TŠ( €€˜˜‚Q€ ‚’ß)ŠsŒ@ 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.ŸjTŠŽ5 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.1sŒCŽ1æ’’’’’’’’9’’’’CŽ(Įé°Ž,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+CŽW( €€˜˜‚Q€ ‚’ň,(Į= H€€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Expansion: Isentropic (Real)This subsection provides analysis of isW(ĮŽentropic 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.1WYĮ1»’’’’’’’’:’’’’YĮćĘé°(ĮBĀ9 @€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+YĮmĀ( €€˜˜‚Q€ ‚’ŽBĀ‹Ä@ 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. čmĀ«Ę8 >€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 temperature and power output values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back to8‹ÄćĘ( € €†Ų”Q€ ’the Main menu.1«ĘĒ1‘’’’’’’’’;’’’’ĒtÉé°ćĘżĒ9 @€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+Ē(Č( €€˜˜‚Q€ ‚’LżĒtÉ; 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(Č„É1’’’’’’’’<’’’’„ÉĪé°tÉŽŹ9 @€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+„ɹŹ( €€˜˜‚Q€ ‚’3šŽŹģĢC 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 defaultć¹ŹĪ2 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.1ģĢ2Ī10’’’’’’’’=’’’’2ĪXé°ĪĻ9 @€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+2ĪFĻ( €€˜˜‚Q€ ‚’ĖĻX; D€—€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Heat TransferThis subsection provides analysis of heat transfer.Input Values:Hot WorkFĻXĪing 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 losses1FĻ‰1Ś’’’’’’’’>’’’’‰2é°Xr9 @€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€ ‚’ßr»? 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.=ų< 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:»2) "€"€†Ų”Q€ ‚’the Main menu.1ųc1’’’’’’’’?’’’’c: é°2L9 @€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+cw( €€˜˜‚Q€ ‚’ƉL: : 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 losses1wk 1W’’’’’’’’@’’’’k ‘é°: T 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+k  ( €€˜˜‚Q€ ‚’ŌT ‘ > J€©€†Ų”Q€‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes: MixingSTEP 1Select the desired inlet species (inlet working fluids) or go with the defaultspecies.STEP 2Enter the desired inlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 3Enter the desired inlet working fluids inlet temperature values or go with thedefault temperature values.STEP 4Enter the desired hot working fluid outlet temperature value or go with theĘ ‘: 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‘ Ā19’’’’’’’’A’’’’Ā[A鰑·@9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’EngiĀ·@‘neering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Āā@( €€˜˜‚Q€ ‚’yK·@[A. ,€–€†Ų”Q€‚€ ‚‚’Compressible FlowThis section provides analysis of compressible flow.1ā@ŒA1P’’’’’’’’B’’’’ŒA«Cé°[AuB9 @€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+ŒA B( €€˜˜‚Q€ ‚’ ÓuB«C8 >€§€†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 BÜC13’’’’’’’’C’’’’ÜCŽFé°«CÅD9 @€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+ÜCšD( €€˜˜‚Q€ ‚’ī²ÅDŽF< 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.1šDG1K’’’’’’’’D’’’’G)Ié°ŽFųG9 @€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+G#H( €€˜˜‚Q€ ‚’ĪųG)I8 >€€†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#HZI1¤’’’’’’’’E’’’’ZIĶLé°)ICJ9 @€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+ZInJ( €€˜˜‚Q€ ‚’%ēCJ“L> 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:nJĶL) "€"€†Ų”Q€ ‚’the Main menu.1“LžL1’’’’’’’’F’’’’žLĶNé°ĶLēM9 @€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+žLN( €€˜˜‚Q€ ‚’»‹ēMĶN0 .€€†Ų”Q€‚€ ‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1NžN1’’’’’’’’G’’’’žNzé°ĶN €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.comžN €ĶN+žN7€( €€˜˜‚Q€ ‚’C  €z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 constant17€«1G’’’’’’’’H’’’’«Į…é°z”‚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‚( €€˜˜‚Q€ ‚’*ź”‚é„@ 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 stagnationŲŖæ‚Į…. *€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.1é„ņ…1|’’’’’’’’I’’’’ņ…=ˆé°Į…Ū†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+ņ…‡( €€˜˜‚Q€ ‚’7’Ū†=ˆ8 >€’€†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‡nˆ1I’’’’’’’’J’’’’nˆ†Œé°=ˆW‰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+nˆ‚‰( €€˜˜‚Q€ ‚’0ņW‰²‹> 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¦‚‰†Œ. *€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.1²‹·Œ1†’’’’’’’’K’’’’·Œ 鰆Œ 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+·ŒĖ( €€˜˜‚Q€ ‚’A   8 >€€†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 constant1Ė=1W’’’’’’’’L’’’’=jĆé° 2Ą9 @€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=2Ą  Site:http://www.engineering-4e.com+=]Ą( €€˜˜‚Q€ ‚’)ė2Ą†Ā> 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]ĄjĆ/ ,€k€†Ų”Q€ ‚‚‚‚‚‚’stagnation temperature and stagnation pressure values for the choseninput values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1†Ā›Ć1K’’’’’’’’M’’’’›ĆµĘé°jĆ„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+›ĆÆÄ( €€˜˜‚Q€ ‚’Ź„ĵĘ< 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 constant1ÆÄęĘ1ß’’’’’’’’N’’’’ęĘ”Ėé°µĘĻĒ9 @€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+ęĘśĒ( €€˜˜‚Q€ ‚’ ĢĻĒŹ> 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_śĒ”Ė1 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.1ŹÅĖ1Š’’’’’’’’O’’’’ÅĖĪ鰔Ė®Ģ9 @€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+ÅĖŁĢ( €€˜˜‚Q€ ‚’E ®ĢĪ8 >€€†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 constant1ŁĢOĪ1y’’’’’’’’P’’’’OĪné°Ī8Ļ9 @€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+OĪcĻ( €€˜˜‚Q€ ‚’Ż8ĻŠ> J€»€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: DiffuserSTEP 1Select the desired working fluid (specie) orcĻŠĪ 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,äµcĻn/ ,€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.1ŠŸ1æ’’’’’’’’Q’’’’Ÿ-é°nˆ9 @€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+Ÿ³( €€˜˜‚Q€ ‚’zAˆ-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 constant1³^1’’’’’’’’R’’’’^G é°-G9 @€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+^r( €€˜˜‚Q€ ‚’.šG > 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§prG 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 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