?_w’’’’,“g^l… 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:"ąš ŃAB R€Į€†Ų”Q€‚€ €‚‚‚‚‚‚‚‚‚‚€ ‚€‚’Thermodynamic and Transp£ŃAS ort 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’·£ŠCH ^€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 constant1ŃAD1>’’’’’’’’’’’’DGė±ŠCģD: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+DE( €€˜˜‚Q€ ‚’÷½ģDG: B€{€†Ų”Q€‚€‚€ €‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Steam Approximations program, theuser needs to change one or more input values 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.1E?G1W’’’’’’’’’’’’?GeMė±G*H: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+?GUH( €€˜˜‚Q€ ‚’5ó*HŠJB R€ē€†Ų”Q€‚€‚€ €‚‚‚‚€ €‚‚‚‚’Limited WarrantyThis software package is sold AS IS, without warranty as to itsperformance. The entire risk as to the quality and of the performanceof this computer software program is assumed by the user.However, to the original purchaser only, Engineering Software warrantsthe medium on which the program is recorded to be free from defects inmaterials and faulty workmanship under normal use and service for aperiod of thirty (30) days from the date of purchase. If during thisAńUHĖLP n€ć€†Ų”Q€‚€ €€ €‚€ €€ €‚‚‚‚‚€ €‚‚’period a defect on the medium should occur, the medium may bereturned to Engineering Software or to an authorized EngineeringSoftware distributor and Engineering Software will replace themedium without charge to you. Your sole and exclusive remedy in theevent of a defect is expressly limited to replacement of the medium asprovided above.If the failure of the medium, in the judgment of Engineering Softwareresulted from accident, abuse or misapplication of the medium, thenšmŠJeM- *€Ś€†Ų”Q€ €‚‚’Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1ĖL–M1’’’’’’’’’’’’–M€ė±eMN: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+–M¬N( €€˜˜‚Q€ ‚’LNųN- *€>€†Ų”Q€‚€‚’Suggestion/Evaluation FormܬN€8 >€¹€ †Ų”Q€‚‚€ ‚€‚‚‚‚‚‚’Please FAX or Mail This Suggestion/Evaluation Form To:Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineerųN€eMing-4e.com‘]ųN©€4 8€ŗ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:@€é€) "€.€ †Ų”Q€ ‚’Steam Approximations—Z©€€= J€“€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Quality:Usefulness:Possible areas of improvement:Other suggestions:1週1j’’’’’’’’’’’’±ź†ė±€œ‚: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+±Ē‚( €€˜˜‚Q€ ‚’ Üœ‚ē„D V€¹€†Ų”Q€‚€‚€ €‚€ €‚‚‚‚‚‚‚‚‚’License AgreementThis software is the property of Engineering Software and is protectedby federal copyright law. While Engineering Software continues to ownthe software, you will have certain rights to use the software after youracceptance of this license. Your rights and obligations with respect tothe use of this software are as follows:You may:- use one copy of the software on a single computer,- make one copy of the software for backup purposes andĻĒ‚ź†4 6€Ÿ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚’- use the software on a network, provided that you have a licensed copy of the software for each computer that can access the software over the networkYou may not:- copy the documentation which accompanies the software,- sublicense, rent or lease any portion of the software and- reverse engineer, decompile, disassemble, modify, translate, make any attempt to discover the source code of the software or create derivative works from the software1ē„‡1³’’’’’’’’’’’’‡Šė±ź†ˆ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‡1ˆ( €€˜˜‚Q€ ‚’߈FŠ6 :€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.1ˆŠ) "€\€†Ų”Q€‚’steam table calculations are not available.1FŠĪŠ1’’’’’’’’’’’’ĪŠ-ė±Š¹‹: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĪŠä‹( €€˜˜‚Q€ ‚’I¹‹-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 constant1ä‹^1„’’’’’’’’ ’’’’^ŽĄļ²-MŽ= H€e€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ€‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+^xŽ( €€˜˜‚Q€ ‚’ āMŽ¤Ą> 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 thxŽ¤Ą-e 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:xŽŽĄ) "€"€†Ų”Q€‚’the Main menu.1¤ĄĮ1‡’’’’’’’’ ’’’’ĮeĆė±ŽĄśĮ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Į%Ā( €€˜˜‚Q€ ‚’@śĮeĆ9 @€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Properties: Enthalpy - PressureThis subsection provides physical properties of the selected specie forassigned enthalpy and pressure.Input Values:Specie, Enthalpy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1%Ā–Ć1—’’’’’’’’ ’’’’–ĆüĘė±eƁÄ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+–ƬÄ( €€˜˜‚Q€ ‚’ŁÄĀĘ= H€³€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Properties: Enthalpy - PressureSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired enthalpy value or go with the default enthalpy value.STEP 3Enter the desired pressure value or go with the default pressure value.STEP 4Click on the Calculate button to start the calculation of the physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:¬ÄüĘ) "€"€†Ų”Q€‚’the Main menu.1ĀĘ-Ē1‚’’’’’’’’ ’’’’-Ē~Éė±üĘČ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+-ĒCČ( €€˜˜‚Q€ ‚’;Č~É8 >€€†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 constant1CČÆÉ1”’’’’’’’’ ’’’’ÆÉĶė±~ɚŹ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ÆÉÅŹ( €€˜˜‚Q€ ‚’ÖšŹŲĢ= 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:ÅŹĶ) "€"€†Ų”Q€‚’the Main menu.1ŲĢCĶ1`’’’’’’’’’’’’CĶ-ė±Ķ.Ī: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+CĶYĪ( €€˜˜‚Q€ ‚’(ķ.Ī; D€Ū€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’CoefficientsFor each reaction specie, the thermodynamic functions specific heat,enthalpy and entropy as functions of temperature are given in the form ofleast squares coefficients as follows:Cp/R = A1 + A2*T + A3*T^2 + A4*T^3 + A5*T^4 [/]H/(R*T) = A1 + A2*T/2 + A3*T^2/3 + A4*T^3/4 + A5*T^4/5 + A6/T [/]S/R = A1*lnT + A2*T + A3*T^2YĪĶ/2 + A4*T^3/3 + A5*T^4/4 + A7 [/]For each specie, two sets of coefficients are included for two adjecent vYĪ-* $€ģ€†Ų”Q€‚‚’temperature intervals, 273 to 1,000 K and 1,000 to 5,000 K. The data havebeen constrained to be equal at 1,000 K.1^1«’’’’’’’’’’’’^Ųė±-I: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+^t( €€˜˜‚Q€ ‚’d,IŲ8 >€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.1t 1’’’’’’’’’’’’ ēė±Ųō: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ ( €€˜˜‚Q€ ‚’Șōē0 .€1€†Ų”Q€‚€‚‚‚’Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.11’’’’’’’’’’’’éė±ē: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+.( €€˜˜‚Q€ ‚’»ƒé8 >€€†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 Properties1. 1Š’’’’’’’’’’’’ s ė±é : B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ 0 ( €€˜˜‚Q€ ‚’ Ģ 9 = 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:0 s ) "€"€†Ų”Q€‚’the Main menu.19 ¤ 1W’’’’’’’’’’’’¤  @ė±s  : B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¤ ŗ ( €€˜˜‚Q€ ‚’Ņ  @> 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.ŗ  @s 1ŗ =@1®’’’’’’’’’’’’=@µBė± @(A: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=@SA( €€˜˜‚Q€ ‚’b,(AµB6 :€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 Properties1SAęB1Y’’’’’’’’’’’’ęBFė±µBŃC: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ęBüC( €€˜˜‚Q€ ‚’ÕŃCF= H€«€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Steam Approximations: Superheated AreaSTEP 1Enter the desired superheated steam temperature value or go with the defaulttemperature value.STEP 2Enter the desired superheated steam pressure value or go with the defaultpressure value.STEP 3Click on the Calculate button to start the calculation of the steamproperties for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1üC?F1 ’’’’’’’’’’’’?FHė±F*G: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+?FUG( €€˜˜‚Q€ ‚’Ĕ*GH0 .€)€†Ų”Q€‚€‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1UGJH1Ī’’’’’’’’’’’’JHēJė±H5I: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+JH`I( €€˜˜‚Q€ ‚’‡N5IēJ9 @€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: CarnotThis subsection provides analysis of the Carnot cycle.Input Values:Heat Addition Temperature, Heat Rejection TemperatureOutput Values:Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Heat addition and rejectionoccur at constant temperature. Specific heat is constant.1`IK1P’’’’’’’’’’’’K7Nė±ēJL: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+K.L( €€˜˜‚Q€ ‚’ ĢL7N= 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.LhN1’’’’’’’’’’’’hNC€ė±7NSO: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+hN~O( €€˜˜‚Q€ ‚’¹‰SOC€0 .€€†Ų”Q€‚€‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle f~OC€7Nor both powergeneration and propulsion applications.1~Ot€1’’’’’’’’’’’’t€I„ė±C€_: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+t€Š( €€˜˜‚Q€ ‚’Ū_ ƒ; 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.©ŠI„* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1 ƒz„1k’’’’’’’’’’’’z„“‰ė±I„e…: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+z„…( €€˜˜‚Q€ ‚’@e…Š‡? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Power (Ideal)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the default䫐…“‰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.1Š‡å‰1’’’’’’’’’’’’剹ė±“‰ŠŠ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+å‰ūŠ( €€˜˜‚Q€ ‚’ŚŠŠ; D€µ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Power (Real)This subsection provides analysis of the Brayton cycle for the powergeneration application.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.©ūŠ¹* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1ź1C’’’’’’’’’’’’ź/Ćė±¹Վ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ź( €€˜˜‚Q€ ‚’?ՎKĮ? 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KĮ¹ or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the default䫏/Ć9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1KĮ`Ć1’’’’’’’’’’’’`ĆJĒė±/ĆKÄ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+`ĆvÄ( €€˜˜‚Q€ ‚’9żKÄÆĘ< 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›qvÄJĒ* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ÆĘ{Ē1p’’’’’’’’’’’’{ĒŗĢė±JĒfČ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+{Ē‘Č( €€˜˜‚Q€ ‚’EfČÖŹ? 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«‘ČŗĢ9 @€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.1ÖŹėĢ1ˆ’’’’’’’’ ’’’’ėĢąė±ŗĢÖĶ: B€c€†Ų”Q€€ƒ‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ėĢĪ( €€˜˜‚Q€ ‚’8üÖĶE< F€ł€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Propulsion (Real)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHVOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flowĪEŗĢ rate is ignored when calculating the gas turbine power›qĪą* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1E1o’’’’’’’’!’’’’Oė±ąü: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+'( €€˜˜‚Q€ ‚’Dük? L€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultä«'O9 @€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.1k€1Ü’’’’’’’’"’’’’€+ ė±Ok: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+€–( €€˜˜‚Q€ ‚’•[k+ : 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.1–\ 1ä’’’’’’’’#’’’’\  ė±+ G : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+\ r ( €€˜˜‚Q€ ‚’ÓG  < 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.Žbr  , (€Ä€†Ų”Q€‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1 @ 1+’’’’’’’’$’’’’@ ö@ė± +: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+@ V( €€˜˜‚Q€‚’*ń+Œ@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 Resolutions, Fuel HHVNumber of Cylinders, Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Pressure,ExVŒ@ haust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel Consumptionj?Vö@+ &€~€†Ų”Q€‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1Œ@'A1·’’’’’’’’%’’’’'A­Gė±ö@B: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+'A=B( €€˜˜‚Q€ ‚’)źBfD? 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=B‡F< F€Ė€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’temperature value.STEP 6Enter the desired number of resolutions value or go with the defaultnumber of resolutions value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the desired number of cylinders value or go with the default numberof cylinders value.STEP 9Enter the desired cylinder stroke value or go with the default cylinderstroke value.STEP 10Enter the desired stroke to diameter value or go with the default stroke&ōfD­G2 2€é€†Ų”Q€‚‚‚‚‚‚‚‚‚’to diameter value.STEP 11Click on the Calculate button to start the calculation of the Otto cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1‡FŽG1ń’’’’’’’’&’’’’ŽGžKė±­GÉH: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŽGōH( €€˜˜‚Q€ ‚’2łÉH&K9 @€ó€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: DieselThis subsection provides analysis of the Diesel cycle.Input Values:Working Fluid, Ambient Temperature, Ambient Pressure, CompressionRatio, Cut-Off Ratio, Number of Resolutions, Fuel HHV, Number of Cylinders,Cylinder Stroke, Stroke to Diameter RatioOutput Values:Compression Temperature, Compression Pressure, Combustion Temperature,Combustion Pressure, Exhaust Temperature, Exhaust Pressure, CycleEfficiency, Working Fluid Mass Flow Rate, Heat Rate, Power Output, FuelxLōHžK, (€˜€†Ų”Q€‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1&KĻK1Ż’’’’’’’’'’’’’ĻKw‚ė±žKŗL: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĻKåL( €€˜˜‚Q€ ‚’/šŗLO? 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,šåLL< F€į€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’cut-off ratio value.STEP 6Enter the desired number of resolutions value or go with the defaultnumber of resolutions value.STEP 7Enter the desired fuel HHV value or go wOLžKith 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+łOw‚2 2€ó€†Ų”Q€‚‚‚‚‚‚‚‚‚’diameter ratio value.STEP 11Click on the Calculate button to start the calculation of the Diesel cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1L؂1•’’’’’’’’(’’’’؂ ‡ė±w‚“ƒ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+؂¾ƒ( €€˜˜‚Q€ ‚’2ł“ƒš…9 @€ó€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: MagnetohydrodynamicsThis subsection provides analysis of the Magnetohydrodynamics cycle.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet Stagnation Pressure,Velocity, Conductivity, Loading Parameter, Magnetic Field Strength,Channel Length, MobilityOutput Values:Inlet Static Temperature, Inlet Static Pressure, Inlet Mach Number,Induced Voltage Field, Current Density, Hall Voltage, Outlet StaticTemperature, Outlet Static Pressure, Outlet Mach Number, Outletķ¾ƒ ‡/ ,€Ū€†Ų”Q€‚‚‚‚‚‚’Stagnation Temperature, Outlet Stagnation Pressure, Specific WorkOutput, Enthalpy ExtractionAssumptions:Specific heat, velocity, conductivity, mobility, induced voltage field, Hallvoltage and magnetic field strength are constant.1š…=‡1S’’’’’’’’)’’’’=‡_ė± ‡(ˆ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=‡Sˆ( €€˜˜‚Q€ ‚’4ö(ˆ‡Š> J€ķ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: MagnetohydrodynamicsSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired inlet stagnation temperature value or go with the defaulttemperature value.STEP 3Enter the desired inlet stagnation pressure value or go with the defaultpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Enter the desired conductivity value or go with the default conductivity value.H SˆĻŒ< F€€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’STEP 6Enter the desired loading parameter value or go with the default loadingparameter value.STEP 7Enter the desired magnetic field strength value or go with the defaultmagnetic field strength value.STEP 8Enter the desired channel length value or go with the default channellength value.STEP 9Enter the desired mobility value or go with the default mobility value.STEP 10Click on the Calculate button to start the calculation of the Magnetohydrodynamics cycle output values for the chosen input values.d‡Š_, (€Č€†Ų”Q€‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1ĻŒ1Ā’’’’’’’’*’’’’-Ąė±_{Ž: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¦Ž( €€˜˜‚Q€ ‚’ß{Ž“/ ,€æ€€‚€‚‚‚‚‚‚‚‚’Power Cycles: Fuel CellThis subsection provides analysis of the Fuel Cell cycle.Input Values:Fuel, Fuel Inlet Temperature, Oxidant (O2) Inlet Temperature,Fuel Flow Rate, Product Outlet TemperatureOutput Values:mD¦Ž-Ą) "€ˆ€†Ų”Q€‚’Oxidant Flow Rate, Fuel Cell Volta“-Ą_ge, Power, Fuel Cell Efficiency1“^Ą1’’’’’’’’+’’’’^Ą¼Äė±-ĄIĮ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+^ĄtĮ( €€˜˜‚Q€ ‚’ įIĮ”Ć? L€Ć€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Fuel CellSTEP 1Select the desired fuel (working fluid) or go with the default selection.STEP 2Enter the desired fuel inlet temperature or go with the defaulttemperature value.STEP 3Enter the desired oxidant inlet temperature value or go with the defaulttemperature value.STEP 4Enter the desired fuel flow rate or go with the default fuel flow ratevalue.STEP 5Enter the desired product outlet temperature value or go with the default(ötĮ¼Ä2 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”ĆķÄ1’’’’’’’’,’’’’ķÄŪĘė±¼ÄŲÅ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ķÄĘ( €€˜˜‚Q€ ‚’ŲØŲÅŪĘ0 .€Q€†Ų”Q€‚€‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1Ę Ē1Ś’’’’’’’’-’’’’ ĒµČė±ŪĘ÷Ē: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ Ē"Č( €€˜˜‚Q€ ‚’“e÷ĒµČ. ,€Ź€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1"ČęČ1ō’’’’’’’’.’’’’ęČ©Ėė±µČŃÉ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ęČüÉ( €€˜˜‚Q€ ‚’­pŃÉ©Ė= 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.1üÉŚĖ1)’’’’’’’’/’’’’ŚĖė±©ĖÅĢ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŚĖšĢ( €€˜˜‚Q€ ‚’ ĒÅĢłĪB 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 5ˆUšĢ3 4€«€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Click on the Calculate button to start the calculation of compressor outlettemperature and power input valułĪ©Ėes for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1łĪ¾1ó’’’’’’’’0’’’’¾€ė±©: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¾Ō( €€˜˜‚Q€ ‚’¬o©€= H€ß€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1Ō±1×’’’’’’’’1’’’’±Wė±€œ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+±Ē( €€˜˜‚Q€ ‚’ĘœĻB 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 5ˆUĒW3 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.1Ļˆ1×’’’’’’’’2’’’’ˆ. ė±Ws : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ˆž ( €€˜˜‚Q€ ‚’Ss . = 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 compression1ž _ 1 ’’’’’’’’3’’’’_  @ė±. J : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+_ u ( €€˜˜‚Q€ ‚’AžJ ¶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 defaultęu  @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.¶ @. 1¶=@1į’’’’’’’’4’’’’=@äAė± @(A: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=@SA( €€˜˜‚Q€ ‚’‘c(AäA. ,€Ę€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1SAB1©’’’’’’’’5’’’’BEė±äAC: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+B+C( €€˜˜‚Q€ ‚’ŁCCE? 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!+CE) "€B€†Ų”Q€‚’Specific heat is not constant.1CE¾E1’’’’’’’’6’’’’¾ELė±E©F: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¾EŌF( €€˜˜‚Q€ ‚’B©FI< 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.%ėŌF;K: B€×€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Furthermore, click on the fuel Normalize button one more time tocalculate the new stoichiometry value for you.STEP 3Enter the desired fuel temperature value or go with the defaulttemperature value.STEP 4Enter the desired oxidant temperature (preheat) value or go with thedefault temperature value.STEP 5Enter the desired oxidant to fuel ratio ( > 1) or go with the default oxidantto fuel ratio.STEP 6Click on the Calculate button to start the calculation of combustion gasÓ¦IL- (€M€†Ų”Q€‚‚‚‚’composition and flame temperature value for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1;K?L1œ’’’’’’’’7’’’’?LŖOė±L*M: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+?LUM( €€˜˜‚Q€ ‚’ Ģ*M`O? L€™€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Combustion: GasThis subsection provides analysis of the combustion process when gasis considered as the fuel.Input Values:Fuel Composition, Fuel Temperature, Oxidant Composition, OxidantTemperature, Oxidant to Fuel RatioOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Stoichiometry, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!UMŖO) "€B€†Ų”Q€‚’Specific heat is not constant.1`OŪO1Ü’’’’’’’’8’’’’ŪO.†ė±ŖOŅ€: B€c€†Ų”QŪOŅ€ŖO€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŪOż€( €€˜˜‚Q€ ‚’7śŅ€4ƒ= H€õ€†Ų”Q€‚ƒ‚ƒ€‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Combustion: GasSTEP 1Enter the desired fuel (gas) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.%ėż€Y…: 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§4ƒ.†. *€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.1Y…_†1Ö’’’’’’’’9’’’’_†ˆė±.†J‡: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+_†u‡( €€˜˜‚Q€ ‚’aJ‡ˆ. ,€Ā€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1u‡5ˆ1ļ’’’’’’’’:’’’’5ˆóŠė±ˆ ‰: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+5ˆK‰( €€˜˜‚Q€ ‚’Øk ‰óŠ= 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.1K‰$‹1’’’’’’’’;’’’’$‹ Ąė±óŠŒ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+$‹:Œ( €€˜˜‚Q€ ‚’ߌYŽ@ N€æ€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Expansion: Isentropic (Ideal)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired turbine/expander inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine/expander inlet pressure value or go with thedefault pressure value.STEP 4Enter the desired turbine/expander outlet pressure value or go with thedefault pressure value.Ÿj:Œ Ą5 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.YŽ ĄóŠ1YŽ=Ą1ļ’’’’’’’’<’’’’=ĄśĀė± Ą(Į: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=ĄSĮ( €€˜˜‚Q€ ‚’§j(ĮśĀ= H€Õ€†Ų”Q€‚ƒ‚ƒ‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1SĮ+Ć1’’’’’’’’=’’’’+ĆžĒė±śĀÄ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com++ĆAÄ( €€˜˜‚Q€ ‚’ŽÄ_Ę@ 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.ŸjAÄžĒ5 8€Õ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter the desired turbine/expander mass flow rate value or go with thedefault mass flow rate value.STEP 6Click on the Calculate button to start the calculation of turbine/expanderoutlet temperature and power output values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1_Ę/Č1“’’’’’’’’>’’’’/Č‘Źė±žĒÉ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+/ČEÉ( €€˜˜‚Q€ ‚’LÉ‘Ź; 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 expansion1EÉĀŹ1’’’’’’’’?’’’’ĀŹ Ļė±‘Ź­Ė: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĀŹŲĖ( €€˜˜‚Q€ ‚’3š­Ė ĪC 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 defaultćŲĖ Ļ2 2€Ē€†Ų”Q€‚‚‚‚‚‚‚‚‚’mass value.STEP 6Click on the Calculate button to start the calculation of turbine outletvalues for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1 ĪQĻ1M’’’’’’’’@’’’’QĻyė± ĻH: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@QĻH Ļengineering-4e.comWeb Site:http://www.engineering-4e.com+QĻs( €€˜˜‚Q€ ‚’ĖHy; D€—€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Heat TransferThis subsection provides analysis of heat transfer.Input Values:Hot Working Fluid (Specie), Hot Working Fluid Mass Flow Rate, HotWorking Fluid Inlet Temperature, Hot Working Fluid Outlet Temperature,Cold Working Fluid (Specie), Cold Working Fluid Mass Flow Rate, ColdWorking Fluid Inlet TemperatureOutput Values:Cold Working Fluid Outlet TemperatureAssumptions:Ideal heat transfer -- no losses1sŖ1Ü’’’’’’’’A’’’’ŖUė±y•: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŖĄ( €€˜˜‚Q€ ‚’ß•Ž? 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.=Ą< 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:ŽU) "€"€†Ų”Q€‚’the Main menu.1†1 ’’’’’’’’B’’’’†_ ė±Uq : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+†œ ( €€˜˜‚Q€ ‚’Ɖq _ : 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 losses1œ  1Ł’’’’’’’’C’’’’ Ä@ė±_ { : B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ ¦ ( €€˜˜‚Q€ ‚’Ō{ ø> 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 theʦ Ä@: 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 CalculatøÄ@_ e 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.1øõ@1Ą’’’’’’’’D’’’’õ@„Bė±Ä@ąA: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+õ@ B( €€˜˜‚Q€ ‚’yKąA„B. ,€–€†Ų”Q€‚€‚‚’Compressible FlowThis section provides analysis of compressible flow.1 BµB1R’’’’’’’’E’’’’µBÖDė±„B C: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+µBĖC( €€˜˜‚Q€ ‚’ Ó CÖD8 >€§€†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 constant1ĖCE15’’’’’’’’F’’’’E Hė±ÖDņE: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+EF( €€˜˜‚Q€ ‚’ī²ņE H< 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.1F€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1RI‰J1¦’’’’’’’’H’’’’‰JžMė±XJtK: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‰JŸK( €€˜˜‚Q€ ‚’%ētKÄM> 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:ŸKžM) "€"€†Ų”Q€‚’the Main menu.1ÄM/N1’’’’’’’’I’’’’/N €ė±žMO: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+/NEO( €€˜˜‚Q€ ‚’»‹O €0 .€€†Ų”Q€‚€‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.EO €žM1EO=€1Š’’’’’’’’J’’’’=€–‚ė± €(: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+=€S( €€˜˜‚Q€ ‚’C (–‚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 constant1SĒ‚1I’’’’’’’’K’’’’Ē‚߆ė±–‚²ƒ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ē‚Żƒ( €€˜˜‚Q€ ‚’*ź²ƒ†@ 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 stagnationŲŖŻƒ߆. *€U€†Ų”Q€‚‚‚‚‚’temperature and stagnation pressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1†‡1~’’’’’’’’L’’’’‡]‰ė±ß†ū‡: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‡&ˆ( €€˜˜‚Q€ ‚’7’ū‡]‰8 >€’€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Properties: StaticThis subsection provides analysis of static properties.Input Values:Working Fluid, Stagnation Temperature, VelocityOutput Values:Static Temperature, Static PressureAssumptions:Specific heat is constant1&ˆŽ‰1K’’’’’’’’M’’’’Ž‰؍ė±]‰yŠ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ž‰¤Š( €€˜˜‚Q€ ‚’0ņyŠŌŒ> 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¦¤Š؍. *€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.1ŌŒŁ1ˆ’’’’’’’’N’’’’Ł<Ąė±ØĎ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŁļŽ( €€˜˜‚Q€ ‚’A Ď<Ą8 >€€†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 ļŽ<Ą؍NumberAssumptions:Specific heat is constant1ļŽmĄ1T’’’’’’’’O’’’’mĄÄė±<ĄXĮ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+mĄƒĮ( €€˜˜‚Q€ ‚’)ėXĮ¬Ć> 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,䵃ĮÄ/ ,€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¬ĆĮÄ1M’’’’’’’’P’’’’ĮÄŻĒė±Ä¬Å: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĮÄ×Å( €€˜˜‚Q€ ‚’Ź¬ÅŻĒ< F€•€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Normal ShockThis subsection provides analysis of normal shock.Input Values:Working Fluid, Inlet Stagnation Temperature, Inlet StagnationPressure, Inlet VelocityOutput Values:Inlet Static Temperature, Inlet StaticPressure, Inlet Mach NumberOutlet Stagnation Temperature, Outlet Stagnation Pressure, OutletVelocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1×ÅČ1į’’’’’’’’Q’’’’Č¾Ģė±ŻĒłČ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Č$É( €€˜˜‚Q€ ‚’ ĢłČ.Ė> J€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Normal ShockSTEP 1Select the desired working fluid (specie) or go with the default selection.STEP 2Enter the desired inlet stagnation temperature value or go with thedefault inlet stagnation temperature value.STEP 3Enter the desired inlet stagnation pressure value or go with the defaultinlet stagnation pressure value.STEP 4Enter the desired inlet velocity value or go with the default velocityvalue.STEP 5_$ɾĢ1 0€æ€†Ų”Q€‚‚‚‚‚‚‚‚’Click on the Calculate button to start the calculation of inlet Machnumber, inlet static temperature, inlet static pressure, outlet Machnumber, outlet velocity, outlet static temperature, and outlet staticpressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1.ĖļĢ1Œ’’’’’’’’R’’’’ļĢJĻė±¾ĢŚĶ: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ļĢĪ( €€˜˜‚Q€ ‚’E ŚĶJĻ8 >€€†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 constant1Ī{Ļ1|’’’’’’’’S’’’’{Ļœė±JĻr: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 5{ĻrJĻ40-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+{Ļ( €€˜˜‚Q€ ‚’Żrø> J€»€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: DiffuserSTEP 1Select the desired working fluid (specie) or go with the default value.STEP 2Enter the desired static temperature value or go with the default statictemperature value.STEP 3Enter the desired static pressure value or go with the default staticpressure value.STEP 4Enter the desired velocity value or go with the default velocity value.STEP 5Click on the Calculate button to start the calculation of Mach number,䵝œ/ ,€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.1øĶ1Į’’’’’’’’T’’’’Ķ]ė±œø: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ķć( €€˜˜‚Q€ ‚’zAø]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 constant1ćŽ1’’’’’’’’U’’’’Žy ė±]y: B€c€†Ų”Q€€ƒ‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ž¤( €€˜˜‚Q€ ‚’.šyŅ > 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§p¤y 7 <€į€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’rate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1Ņ Ŗ 1]’’’’’’’’V’’’’Ŗ Ö ,y Ö ) "€€†Ų”Q€‚’1Ŗ ’’’’1’’’’’’’’W’’’’’’’’’’’’ 22wT1Helv&ˆC‹v 9\'~év’Tms RmnFō^_‹å]ŹU‹Symbol^‰^ų&öt"&‹CourierŲ-Ś@Ä^ &Times New Romanč-@Arial&ĒGƒFÄ^ƒMS Serif‰Fō‰VöŠFō%MS Sans Serif&‰GŠTimes‰O ŠN÷ƒį ŠéŠé&HelveticaÓź&‰W ĄtSystemt$&‹&‹WŃźŃCourier New‰G&‰WƒRoman&‹Ńč-@Ä^ &‰GScriptƒFėÄ^ +Ą&ModernöFöt[Ä^&öMarlett@Ä^ &‰GƒFArial CE*ä-@Ä^ &‰GArial CYR^™RPÄv &‹DArial Greek<9¢Ä^ &‰Arial TURöFöt[ÄArial Balticg*æ&‹G)Courier New CE)FŽF Courier New CYR-„‹FCourier New GreekWVCourier New TURé–Courier New BalticƒLucida Console|Lucida Sans UnicodeTimes New Roman CETimes New Roman CYRTimes New Roman GreTimes New Roman TURTimes New Roman BalWingdingsĮ‹Ų&€?wƒVerdanaų¹”©ŽŁ^_‹å]ŹArial Black‹ū&€?uComic Sans MSv &ŠŽGeorgiaÄ^&öt#&‹Franklin Gothic MedPalatino Linotype@Tahoma&ĒDƒFŽF Trebuchet MSt&‹ŃčWebdingsėV&ŠŠč*Estrangelo EdessaŠGautami’FÄ^&‹&‹WLatha&‰TƒF&€ŽFžHanzel Condensed· ĄHanzel Extended’všHanzel Ž0&ĒŌ ŽHanzel ThinŹ U‹ģŽHanzel Wide&‹G 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