?_{˙˙˙˙vŽkblф € ‰€ ‚€ƒă? € ‰€ ‚€ƒă@ € ‰€ ‚˙Temperature - PressureEnthalpy - PressureEntropy - Pressure@K/. ,€$€°˜ă€‰€‚˙Power Cycles^ďB T€8€˜€ƒă°€ ‰€ ‚€ƒăą€ ‰€ ‚˙CarnotBrayton˝[/Jb ”€ś€Œ€ƒƒănŤ€ ‰€ ‚€ƒƒăoŤ€ ‰€ ‚€ ƒƒăpŤ‰€ ‚€ ƒƒăqŤ‰€ ‚˙Power (Ideal)Power (Real)Propulsion (Ideal)Propulsion (Real)n$¸J d€H€˜€ ƒă˛‰€ ‚€ ƒăł‰€ ‚€ ƒă´‰€ ‚˙RankineOttoDieselT&J . ,€L€°˜ă€‰€‚˙Power Cycle Components/ProcessesD¸P1 2€&€˜€ƒăé€ ‰€ ‚˙CompressionC ŕM j€†€Œ€ ƒƒăćB߉€ ‚€ ƒƒăçB߉€ ‚€ ƒƒăčB߉€ ‚˙Isentropic (Ideal)Isentropic (Real)Isothermal?P. ,€"€˜€ ƒăꉀ ‚˙CombustionXŕw> L€4€Œ€ ƒƒăJ߉€ ‚€ ƒƒă J߉€ ‚˙Coal/OilGas>ľ. ,€ €˜€ ƒă뉀 ‚˙ExpansionCwEM j€†€Œ€ ƒƒăXQ߉€ ‚€ ƒƒăYQ߉€ ‚€ ƒƒăZQ߉€ ‚˙Isentropic (Ideal)Isentropic (Real)IsothermalEľŠ. ,€.€°˜ă€‰€‚˙Compressible Flowƒ9E J d€r€˜€ ƒă"&‰€ ‚€ ƒă#&‰€ ‚€ ƒă$&‰€ ‚˙Velocity of SoundMach NumberProperties]Šj> L€>€Œ€ ƒƒă |‰€ ‚€ ƒƒă |‰€ ‚˙StagnationStatic‘9 űX €€r€˜€ ƒă%&‰€ ‚€ ƒă&&‰€ ‚€ ƒă'&‰€ ‚€ ƒă(&‰€ ‚˙NozzleNormal ShockDiffuserThrust1j, 1e ˙˙˙˙˙˙˙˙˙˙˙˙, lCé°ű 9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙Ů U < F€ł€€‚€ ‚€ € ‚€ € ‚‚‚‚‚‚‚˙Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Power and Propulsion Systems Analysis, that quickly andreliably calculates thermodynamic and transport properties of gaseous,liquid and solid species, analyzes power cycles, power cyclecomponents/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 ofŮ@ i; D€ł€€ ‚‚‚‚‚‚€ € € € ‚‚€ ‚˙power and propulsion 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 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 PropertiesšU ’@d –€s€€ ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚ƒ‚‚€ ‚˙Temperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureEntropy and PressurePower CyclesCarnotBrayton (Power and Propulsion)RankineOttoDieselPower Cycle Components/ProcessesCompressionCombustion (Coal/Oil/Gas)ExpansionCompressible FlowVelocity of SoundMach Ni’@űumberProperties (Stagnation and Static)NozzleNormal ShockDiffuserThrustHardware Requirements and Software Compatibilityei!A* $€Ę€€ ƒ‚ƒ‚ƒ‚ƒ‚˙80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:j:’@‹A0 0€t€‘€†üEĄ€ ƒƒ‚ƒƒ‚˙Windows 98, Windows 2000, Windows ME andWindows XP ß!A–B, &€ż€€ ‚‚‚‚‚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.ÖĽ‹AlC1 0€K€€ ‚€ ‚€ ‚‚‚‚‚‚˙Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1–BC1o˙˙˙˙˙˙˙˙˙˙˙˙CŰJé°lC†D9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+CąD( €€˜˜‚Q€ ‚˙ ˆDşF> J€—€†ŘĄQ€‚€ ‚€ € ‚‚‚‚‚‚‚‚‚‚˙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:"ŕąDÜHB R€Á€†ŘĄQ€ ‚€ € ‚‚‚‚‚‚‚‚‚‚€ ‚€ ‚˙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˙ˇşFŰJH ^€o€†ŘĄQ€ ‚‚‚‚‚€ € ‚‚‚‚‚‚€ ‚€ ‚‚‚€ ‚˙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 constant1ÜH K1N˙˙˙˙˙˙˙˙˙˙˙˙ K)Né°ŰJőK9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙ ÎőK)N; D€€†ŘĄQ€‚€ ‚€ € ‚‚‚‚‚‚˙How to Use the ProgramIn each section, subsection of the Power and Propulsion SystemsAnalysis program, the user needs to change one or more input valuesin order to calculate a new case. Input values are in boxes with whitebackground and can be changed by clicking on each individual box oreven by using the arrow keys and changing the current value. Outputvalues cannot be modified, changed by the user and they are in boxeswith black background.1 LZN1ą˙˙˙˙˙˙˙˙˙˙˙˙ZNćé°)NCO9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ZNnO( €€˜˜‚Q€ ‚˙ßCO6 :€ż€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚˙PropertiesThis section provides physical properties of available species forassigned twnO)No 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.nOć) "€\€†ŘĄQ€ ‚˙steam table calculations are not available.1‚1Ž˙˙˙˙˙˙˙˙˙˙˙˙‚t„é°ćƒ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙Iƒt„9 @€!€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙Properties: Temperature - PressureThis subsection provides physical properties of the selected specie forassigned temperature and pressure.Input Values:Specie, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1+ƒĽ„1Ł˙˙˙˙˙˙˙˙˙˙˙˙Ľ„ˆíąt„’…< F€c€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ€ ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ľ„˝…( €€˜˜‚Q€ ‚˙ â’…݇> J€Ĺ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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:˝…ˆ) "€"€†ŘĄQ€ ‚˙the Main menu.1݇Hˆ1…˙˙˙˙˙˙˙˙˙˙˙˙HˆœŠé°ˆ1‰9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Hˆ\‰( €€˜˜‚Q€ ‚˙@1‰œŠ9 @€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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\‰ÍŠ1•˙˙˙˙˙˙˙˙˙˙˙˙͊1Žé°œŠś‹9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+͊á‹( €€˜˜‚Q€ ‚˙Ůś‹÷= H€ł€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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:á‹1Ž) "€"€†ŘĄQ€ ‚˙the Main menu.1÷bŽ1€˙˙˙˙˙˙˙˙ ˙˙˙˙bŽ˝Ŕé°1ŽK9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+bŽv( €€˜˜‚Q€ ‚˙;K˝Ŕ8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙Properties: Entropy - PressureThis subsection provides physical properties ofv˝Ŕ1Ž the selected specie forassigned entropy and pressure.Input Values:Specie, Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1vîŔ1’˙˙˙˙˙˙˙˙ ˙˙˙˙îŔOÄé°˝Ŕ×Á9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+îŔÂ( €€˜˜‚Q€ ‚˙Ö×ÁÄ= H€­€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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:ÂOÄ) "€"€†ŘĄQ€ ‚˙the Main menu.1ĀÄ1 ˙˙˙˙˙˙˙˙ ˙˙˙˙€Ä\Čé°OÄiĹ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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”Ĺ( €€˜˜‚Q€ ‚˙(íiĹźÇ; D€Ű€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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”Ĺ\Č* $€ě€†ŘĄQ€ ‚‚˙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.1źÇČ1Š˙˙˙˙˙˙˙˙ ˙˙˙˙ČËé°\ČvÉ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ČĄÉ( €€˜˜‚Q€ ‚˙d,vÉË8 >€Y€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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.1ĄÉ6Ë1 ˙˙˙˙˙˙˙˙ ˙˙˙˙6ËÍé°ËĚ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+6ËJĚ( €€˜˜‚Q€ ‚˙ȘĚÍ0 .€1€†ŘĄQ€‚€ ‚‚‚˙Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1JĚCÍ1˙˙˙˙˙˙˙˙˙˙˙˙CÍé°Í,Î9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+CÍWÎ( €€˜˜‚Q€ ‚˙ťƒ,Î8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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 PhyWÎÍsical Properties1WÎO1ˆ˙˙˙˙˙˙˙˙˙˙˙˙OŚé°89 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Oc( €€˜˜‚Q€ ‚˙ Ě8l= H€™€†ŘĄQ€‚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:cŚ) "€"€†ŘĄQ€ ‚˙the Main menu.1l×1U˙˙˙˙˙˙˙˙˙˙˙˙×űé°ŚŔ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+×ë( €€˜˜‚Q€ ‚˙ŇŔű> J€Ľ€†ŘĄQ€‚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.1ë,1§˙˙˙˙˙˙˙˙˙˙˙˙,˘ é°ű9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙b,˘ 6 :€Y€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚˙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 Properties1@Ó 1W˙˙˙˙˙˙˙˙˙˙˙˙Ó ů é°˘ ź 9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ó ç ( €€˜˜‚Q€ ‚˙Őź ů = H€Ť€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.1ç * 1ç˙˙˙˙˙˙˙˙˙˙˙˙* ŕé°ů 9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙˘sŕ/ .€ć€†ŘĄQ€‚€ ‚‚‚˙Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto and Diesel).1>1Ě˙˙˙˙˙˙˙˙˙˙˙˙žAé°ŕ @9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com @ŕ+7@( €€˜˜‚Q€ ‚˙‡N @žA9 @€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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.17@ďA1N˙˙˙˙˙˙˙˙˙˙˙˙ďA Eé°žAŘB9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ďAC( €€˜˜‚Q€ ‚˙ ĚŘB E= H€™€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.1C=E1ţ˙˙˙˙˙˙˙˙˙˙˙˙=E Gé° E&F9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=EQF( €€˜˜‚Q€ ‚˙š‰&F G0 .€€†ŘĄQ€‚€ ‚‚‚˙Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1QF;G1˙˙˙˙˙˙˙˙˙˙˙˙;GKé° G$H9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+;GOH( €€˜˜‚Q€ ‚˙Ű$HeJ; D€ˇ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.ŠOHK* $€ţ€†ŘĄQ€ ‚‚˙Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1eJ?K1Ş˙˙˙˙˙˙˙˙˙˙˙˙?Kƒ€é°K(L9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+?KSL( €€˜˜‚Q€ ‚˙@(L“N? L€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 defaultäŤSLƒ€9 @€W€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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“Nƒ€K chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1“N´€1\˙˙˙˙˙˙˙˙˙˙˙˙´€߄鰃€9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+´€ȁ( €€˜˜‚Q€ ‚˙۝܃9 @€ˇ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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 RateŐȁ߄. *€Ť€†ŘĄQ€ ‚‚‚‚‚˙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܃…1î˙˙˙˙˙˙˙˙˙˙˙˙…͋é°ß„ů…9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙?ů…cˆ? L€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 defaultA$†¤Š< F€ €†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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)÷cˆ͋2 2€ď€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙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.1¤Šţ‹1˙˙˙˙˙˙˙˙˙˙˙˙ţ‹ Ŕé°Í‹çŒ9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ţ‹( €€˜˜‚Q€ ‚˙9ýçŒK< F€ű€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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›q Ŕ* $€â€†ŘĄQ€ ‚‚˙output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.K Ŕ͋1K=Ŕ1t˙˙˙˙˙˙˙˙˙˙˙˙=ŔzĹé° Ŕ&Á9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=ŔQÁ( €€˜˜‚Q€ ‚˙E&Á–Ă? L€ €†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 defaultäŤQÁzĹ9 @€W€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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–ĂŤĹ1o˙˙˙˙˙˙˙˙˙˙˙˙ŤĹéÉé°zĹ”Ć9 @€a€†ŘĄQ€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŤĹżĆ( €€˜˜‚Q€ ‚˙I ”ĆÉ< F€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.áśżĆéÉ+ $€m€†ŘĄQ€ ‚‚˙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.1ÉĘ1y˙˙˙˙˙˙˙˙˙˙˙˙Ęĺé°éÉË9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ę.Ë( €€˜˜‚Q€ ‚˙DËrÍ? L€ €†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 defaultA.ËłĎ< F€ €†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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&őrÍĺ1 0€ë€†ŘĄQ€ ‚‚‚‚‚‚‚‚˙efficiency value.STEP 11łĎĺéÉClick 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.1łĎ1Ú˙˙˙˙˙˙˙˙˙˙˙˙żé°ĺ˙9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙•[˙ż: B€ˇ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚˙Power Cycles: RankineThis subsection provides analysis of the Rankine cycle.Input Values:Turbine Inlet Conditions (Temperature and Pressure), Steam Mass FlowRate, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion and heattransfer.1*đ1â˙˙˙˙˙˙˙˙ ˙˙˙˙đĄé°żŮ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+đ( €€˜˜‚Q€ ‚˙ÓŮ< F€§€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.ŽbĄ, (€Ä€†ŘĄQ€ ‚‚‚‚˙STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1Ň1Ů˙˙˙˙˙˙˙˙!˙˙˙˙Ňz é°Ąť9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ňć( €€˜˜‚Q€‚˙*ńť 9 @€ă€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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?ćz + &€~€†ŘĄQ€ ‚‚‚˙Assumptions:Specific heat is constant. Four stroke engine.1 Ť 1t˙˙˙˙˙˙˙˙"˙˙˙˙Ť ;Bé°z ” 9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ť ż ( €€˜˜‚Q€ ‚˙)ę” č? L€Ő€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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!ĺż A< F€Ë€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 čAz 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&ôč;B2 2€é€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙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.1AlB1ď˙˙˙˙˙˙˙˙#˙˙˙˙lB*Fé°;BUC9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+lB€C( €€˜˜‚Q€ ‚˙2ůUC˛E9 @€ó€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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, FuelxL€C*F, (€˜€†ŘĄQ€ ‚‚‚‚˙ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1˛E[F1Ë˙˙˙˙˙˙˙˙$˙˙˙˙[FőLé°*FDG9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+[FoG( €€˜˜‚Q€ ‚˙/đDGžI? L€á€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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,đoGĘK< F€á€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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+ůžIőL2 2€ó€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙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.1ĘK&M1ľ˙˙˙˙˙˙˙˙%˙˙˙˙&M”é°őLN9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+&M:N( €€˜˜‚Q€ ‚˙2ůNx€9 @€ó€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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, Cu:Nx€őLrrent Density, Hall Voltage, Outlet StaticTemperature, Outlet Static Pressure, Outlet Mach Number, Outletí:N”/ ,€Ű€†ŘĄQ€ ‚‚‚‚‚‚˙Stagnation Temperature, Outlet Stagnation Pressure, Specific WorkOutput, Enthalpy ExtractionAssumptions:Specific heat, velocity, conductivity, mobility, induced voltage field, Hallvoltage and magnetic field strength are constant.1x€Ł1Q˙˙˙˙˙˙˙˙&˙˙˙˙Łĺ‡鰔Ž‚9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Łق( €€˜˜‚Q€ ‚˙4öŽ‚ …> J€í€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 قU‡< F€€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 …ĺ‡, (€Č€†ŘĄQ€ ‚‚‚‚˙STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1U‡ˆ1Ŕ˙˙˙˙˙˙˙˙'˙˙˙˙ˆĽŠé°ĺ‡˙ˆ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙ß˙ˆ8Š/ ,€ż€€‚€ ‚‚‚‚‚‚‚‚˙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*‰ĽŠ) "€ˆ€†ŘĄQ€ ‚˙Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency18Š֊1˙˙˙˙˙˙˙˙(˙˙˙˙֊2é°ĽŠż‹9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+֊ę‹( €€˜˜‚Q€ ‚˙ áż‹ Ž? L€Ă€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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(öę‹22 2€í€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙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 Žc1"˙˙˙˙˙˙˙˙)˙˙˙˙cDÁé°2XŔ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-36cXŔ205E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+cƒŔ( €€˜˜‚Q€ ‚˙Á‘XŔDÁ0 .€#€†ŘĄQ€‚€ ‚‚‚˙Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).1ƒŔuÁ1Ř˙˙˙˙˙˙˙˙*˙˙˙˙uÁĂé°DÁ^Â9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+uÁ‰Â( €€˜˜‚Q€ ‚˙“e^ÂĂ. ,€Ę€†ŘĄQ€‚€ ‚‚˙Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1‰ÂMĂ1ň˙˙˙˙˙˙˙˙+˙˙˙˙MĂĆé°Ă6Ä9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+MĂaÄ( €€˜˜‚Q€ ‚˙­p6ÄĆ= H€á€†ŘĄQ€‚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.1aÄ?Ć1Ö˙˙˙˙˙˙˙˙,˙˙˙˙?ĆäĘé°Ć(Ç9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+?ĆSÇ( €€˜˜‚Q€ ‚˙ Ç(Ç\ÉB R€€†ŘĄQ€‚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 5ˆUSÇäĘ3 4€Ť€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚˙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\ÉË1˙˙˙˙˙˙˙˙-˙˙˙˙ËřÍé°äĘţË9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ë)Ě( €€˜˜‚Q€ ‚˙Ď‘ţËřÍ> J€#€†ŘĄQ€‚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)Ě)Î1l˙˙˙˙˙˙˙˙.˙˙˙˙)Î[é°řÍĎ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+)Î=Ď( €€˜˜‚Q€ ‚˙ĆĎQB R€€†ŘĄQ€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes:Compression: Isentropic (Real)STEP 1Select the desired specie or go with th=ĎQřÍe 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 Ô=Ď[6 :€Š€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.1QŒ1Ő˙˙˙˙˙˙˙˙/˙˙˙˙Œ0é°[u9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙Su0= H€§€†ŘĄQ€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processs:Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid (Specie), Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression1 a1ž˙˙˙˙˙˙˙˙0˙˙˙˙aÎ é°0J9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+au( €€˜˜‚Q€ ‚˙AţJś C T€ý€†ŘĄQ€‚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 defaultćuÎ 2 2€Í€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙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.1ś ˙ 1Ö˙˙˙˙˙˙˙˙1˙˙˙˙˙ ¤ é°Î č 9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙‘cč ¤ . ,€Ć€†ŘĄQ€‚€ ‚‚˙Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1 Ő 1Â˙˙˙˙˙˙˙˙2˙˙˙˙Ő W@é°¤ ž 9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ő é ( €€˜˜‚Q€ ‚˙Ůž  @? L€ł€†ŘĄQ€‚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.é  @¤ J!é W@) "€B€†ŘĄQ€ ‚˙Specific heat is not constant.1 @ˆ@1˙˙˙˙˙˙˙˙3˙˙˙˙ˆ@ÖFé°W@qA9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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@œA( €€˜˜‚Q€ ‚˙BqAŢC< F€ €†ŘĄQ€‚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.%ëœAF: B€×€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 gasÓŚŢCÖF- (€M€†ŘĄQ€ ‚‚‚‚˙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.1FG1š˙˙˙˙˙˙˙˙4˙˙˙˙GpJé°ÖFđG9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+GH( €€˜˜‚Q€ ‚˙ ĚđG&J? L€™€†ŘĄQ€‚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!HpJ) "€B€†ŘĄQ€ ‚˙Specific heat is not constant.1&JĄJ1|˙˙˙˙˙˙˙˙5˙˙˙˙ĄJň€é°pJŠK9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĄJľK( €€˜˜‚Q€ ‚˙7úŠKěM= H€ő€†ŘĄQ€‚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.%ëľK€: B€×€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 ofěM€pJ combustion gasŐ§ěMň€. *€O€†ŘĄQ€ ‚‚‚‚‚˙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€#1Ô˙˙˙˙˙˙˙˙6˙˙˙˙#Ƃé°ň€ ‚9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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‚( €€˜˜‚Q€ ‚˙a ‚Ƃ. ,€Â€†ŘĄQ€‚€ ‚‚˙Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.17‚÷‚1í˙˙˙˙˙˙˙˙7˙˙˙˙÷‚ł…é°Ć‚ŕƒ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙¨kŕƒł…= H€×€†ŘĄQ€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙Power CycleComponents/Processes:Expansion: Isentropic (Ideal)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1 „ä…1˙˙˙˙˙˙˙˙8˙˙˙˙ä…śŠé°ł…͆9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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…ř†( €€˜˜‚Q€ ‚˙ß͆‰@ N€ż€†ŘĄQ€‚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.Ÿjř†śŠ5 8€Ő€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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‰çŠ1 ˙˙˙˙˙˙˙˙9˙˙˙˙çŠŔé°śŠЋ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+çŠű‹( €€˜˜‚Q€ ‚˙ĹˆЋŔ= H€€†ŘĄQ€‚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.1ű‹ń1Ž˙˙˙˙˙˙˙˙:˙˙˙˙ń‡Ăé°Ŕڎ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ń( €€˜˜‚Q€ ‚˙Ţڎ/Á@ N€˝€†ŘĄQ€‚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 /ÁŔ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. čOĂ8 >€Ń€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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/Á‡Ă( € €†ŘĄQ€ ˙the Main menu.1OøĂ1‘˙˙˙˙˙˙˙˙;˙˙˙˙¸ĂĆ鰇ĂĄÄ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¸ĂĚÄ( €€˜˜‚Q€ ‚˙LĄÄĆ; D€#€†ŘĄQ€‚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 expansion1ĚÄIĆ1˙˙˙˙˙˙˙˙<˙˙˙˙IĆĽĘé°Ć2Ç9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+IĆ]Ç( €€˜˜‚Q€ ‚˙3đ2ǐÉC T€á€†ŘĄQ€‚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 defaultă]ÇĽĘ2 2€Ç€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚˙mass value.STEP 6Click on the Calculate button to start the calculation of turbine outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1ÉÖĘ1K˙˙˙˙˙˙˙˙=˙˙˙˙ÖĘđÍé°ĽĘżË9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ÖĘęË( €€˜˜‚Q€ ‚˙ËżËđÍ; D€—€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 losses1ęË!Î1ý˙˙˙˙˙˙˙˙>˙˙˙˙!ÎÖé°đÍ Ď9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+!Î5Ď( €€˜˜‚Q€ ‚˙ß Ď_? L€ż€†ŘĄQ€‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Power CycleComponents/Processes: Heat TransferSTEP 1Select the desired hot specie (hot working fluid) or go with the def5Ď_đÍaultspecie.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.=5Ďœ< F€€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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:_Ö) "€"€†ŘĄQ€ ‚˙the Main menu.1œ1˙˙˙˙˙˙˙˙?˙˙˙˙Ţé°Öđ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙ÉđŢ: B€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 losses11W˙˙˙˙˙˙˙˙@˙˙˙˙5 é°Ţř9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙Ôř5 > J€Š€†ŘĄQ€‚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 theĆ#5 : B€€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.15 f 1ž˙˙˙˙˙˙˙˙A˙˙˙˙f ó é°5 O 9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+f z ( €€˜˜‚Q€ ‚˙yKO ó . ,€–€†ŘĄQ€‚€ ‚‚˙Compressible FlowThis section provides analysis of compressible flow.1z $1c˙˙˙˙˙˙˙˙B˙˙˙˙$O@é°ó  9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙ Ó O@8 >€§€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Velocity of SoundThis section provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput 8O@ó Values:Velocity of SoundAssumptions:Specific heat is constant18€@13˙˙˙˙˙˙˙˙C˙˙˙˙€@‚Cé°O@iA9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+€@”A( €€˜˜‚Q€ ‚˙î˛iA‚C< F€e€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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.1”AłC1K˙˙˙˙˙˙˙˙D˙˙˙˙łCÍE鰂CœD9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+łCÇD( €€˜˜‚Q€ ‚˙ΜDÍE8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1ÇDţE1¤˙˙˙˙˙˙˙˙E˙˙˙˙ţEqIé°ÍEçF9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ţEG( €€˜˜‚Q€ ‚˙%ççF7I> J€Ď€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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:GqI) "€"€†ŘĄQ€ ‚˙the Main menu.17I˘I1˙˙˙˙˙˙˙˙F˙˙˙˙˘IqKé°qI‹J9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+˘IśJ( €€˜˜‚Q€ ‚˙ť‹‹JqK0 .€€†ŘĄQ€‚€ ‚‚‚˙Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1śJ˘K1ˆ˙˙˙˙˙˙˙˙G˙˙˙˙˘KůMé°qK‹L9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+˘KśL( €€˜˜‚Q€ ‚˙C ‹LůM8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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 constant1śL*N1˙˙˙˙˙˙˙˙H˙˙˙˙*NL‚é°ůMO9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙*ęOt@ N€Ő€†ŘĄQ€‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙Running - Compressible Flow:Properties: StagnationSTEP 1Select the desired working fluid (specie) or go with the default>OtůM 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 stagnationŘŞ>OL‚. *€U€†ŘĄQ€ ‚‚‚‚‚˙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.1t}‚1|˙˙˙˙˙˙˙˙I˙˙˙˙}‚Ȅé°L‚fƒ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙7˙fƒȄ8 >€˙€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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‘ƒů„1I˙˙˙˙˙˙˙˙J˙˙˙˙ů„‰é°Č„â…9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ů„ †( €€˜˜‚Q€ ‚˙0ňâ…=ˆ> J€ĺ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 staticÔŚ †‰. *€M€†ŘĄQ€ ‚‚‚‚‚˙temperature and static pressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1=ˆB‰1†˙˙˙˙˙˙˙˙K˙˙˙˙B‰—‹é°‰+Š9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+B‰VŠ( €€˜˜‚Q€ ‚˙A +Š—‹8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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 constant1VŠȋ1R˙˙˙˙˙˙˙˙L˙˙˙˙ȋ Ŕ鰗‹ąŒ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ȋ܌( €€˜˜‚Q€ ‚˙)ëąŒ> J€×€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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,äľÜŒ Ŕ/ ,€k€†ŘĄQ€ ‚‚‚‚‚‚˙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. Ŕ—‹1=Ŕ1N˙˙˙˙˙˙˙˙M˙˙˙˙=ŔWĂé° Ŕ&Á9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=ŔQÁ( €€˜˜‚Q€ ‚˙Ę&ÁWĂ< F€•€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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 constant1QÁˆĂ1ß˙˙˙˙˙˙˙˙N˙˙˙˙ˆĂ6Čé°WĂqÄ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ˆĂœÄ( €€˜˜‚Q€ ‚˙ ĚqÄŚĆ> J€™€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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_œÄ6Č1 0€ż€†ŘĄQ€ ‚‚‚‚‚‚‚‚˙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.1ŚĆgČ1Š˙˙˙˙˙˙˙˙O˙˙˙˙gČŔĘé°6ČPÉ9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+gČ{É( €€˜˜‚Q€ ‚˙E PÉŔĘ8 >€€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚˙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 constant1{ÉńĘ1D˙˙˙˙˙˙˙˙P˙˙˙˙ńĘĎé°ŔĘÚË9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ńĘĚ( €€˜˜‚Q€ ‚˙ÝÚË Î> J€ť€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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,äľĚĎ/ ,€k€†ŘĄQ€ ‚‚‚‚‚‚˙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 Î5Ď1Á˙˙˙˙˙˙˙˙Q˙˙˙˙5ĎĎé°Ď*9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:h5Ď*Ďttp://www.engineering-4e.com+5ĎU( €€˜˜‚Q€ ‚˙zA*Ď9 @€ƒ€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚˙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 constant1U1˙˙˙˙˙˙˙˙R˙˙˙˙éé°Ďé9 @€a€†ŘĄQ€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚˙Engineering 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€ ‚˙.đéB> J€á€†ŘĄQ€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙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§pé7 <€á€†ŘĄQ€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚˙rate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 8When done with Steps 1 through 7, click on the 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