?_|’’’’7ˆlclč„ € ‰€ ‚€ƒć? € ‰€ ‚€ƒć@ € ‰€ ‚’Temperature - PressureEnthalpy - PressureEntropy - PressureH.. ,€4€°˜ć€‰€‚’Steam Approximationso-Ņ‰B T€Z€˜€ƒćw€ ‰€ ‚€ƒćx€ ‰€ ‚’Saturated AreaSuperheated Area1ŗ1" ’’’’’’’’’’’’ŗ« 鰉£9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŗĪ( €€˜˜‚Q€ ‚’-ń£ū< F€ć€€‚€ ‚€ € ‚€ € ‚‚‚‚‚‚‚’Program DescriptionEngineering Software has developed a new Windows based softwarepackage, Physical Properties and Steam Approximations, thatquickly and reliably calculates thermodynamic and transport propertiesof gaseous, liquid and solid species and steam approximations.This software package should prove to be a good tool for those who areinvolved at various levels with design, operation and management ofenergy conversion systems. It should provide you with the opportunity×Ī A P€Æ€€ ‚‚‚‚‚€ € € € ‚‚€ ‚€ ƒ‚ƒ‚’to 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 PropertiesTemperature and Pressure (270 K < T < 5,000 K)Enthalpy and PressureOūb A P€€€ ƒ‚‚€ ‚€ ƒ‚ƒ‚‚€ ‚€ ƒ‚ƒ‚ƒ‚ƒ‚’Entropy and PressureSteam ApproximationsSaturated Area (Temperature and Pressure Dependent)Superheated AreaHardware Requirements and Software Compatibility80486 or higher microprocessor16 MB RAM10 MB available on hard driveIBM compatible systems:h: Ź . ,€t€†üE”€ ƒƒ‚ƒƒ‚’Windows 98, Windows 2000, Windows ME andWindows XP ßb Õ , &€æ€€ ‚‚‚‚‚ƒ‚‚‚’Distributed on CD ROMFree Technical and Product Support30 Day Money Back GuaranteeTrademarks:All product names, company names andservice marks are trademarks or registered trademarks of theirrespective companies.Ö„Ź « 1 0€K€€ ‚€ ‚€ ‚‚‚‚‚‚’Engineering SoftwareP.O. Box 1180Germantown, MD 20875Phone: (301) 540-3605FAX: (301) 540-3605E-Mail: info@engineering-4e.comhttp://www.engineering-4e.com1Õ Ü 1o’’’’’’’’’’’’Ü -Dé°« Å 9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ü š ( €€˜˜‚Q€ ‚’ ĖÅ @> 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:š @« "ąš .BB R€Į€†Ų”Q€ ‚€ € ‚‚‚‚‚‚‚‚‚‚€ ‚€ ‚’Thermodynamic and Transport PropertiesSingle specie considerationIdeal gas approach is used (pv=RT)Specific heat is not constantCoefficients describing thermodynamic and transport propertieswere obtained from the NASA Glenn Research Center at LewisField in Center in Cleveland, OH -- such coefficients conform withthe standard reference temperature of 298.15 K (77 F) and theJANAF tablesPower CyclesSingle specie consideration -- fuel mass flow rate ignored and’· @-DH ^€o€†Ų”Q€ ‚‚‚‚‚€ € ‚‚‚‚‚‚€ ‚€ ‚‚‚€ ‚’its impact on the properties of the working fluidBasic equations hold (continuity, momentum and energyequations)Specific heat is constantPower Cycle Components/ProcessesSingle specie considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constantCompressible FlowSingle specie considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constant1.B^D1U’’’’’’’’’’’’^D‚Gé°-DGE9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+^DrE( €€˜˜‚Q€ ‚’ÕGE‚G; D€«€†Ų”Q€‚€ ‚€ ‚€ ‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Physical Properties and SteamApproximations program, the user needs to change one or moreinput values in order to calculate a new case. Input values are inboxes with white background and can be changed by clicking oneach individual box or even by using the arrow keys and changingthe current value. Output values cannot be modified, changed bythe user and they are in boxes with black background.1rE³G1±’’’’’’’’’’’’³G3K鰂GœH9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+³GĒH( €€˜˜‚Q€ ‚’ßœHÜJ6 :€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.ĒH3K) "€\€†Ų”Q€ ‚’steam table calculations are not available.1ÜJdK1Ž’’’’’’’’’’’’dKĮMé°3KML9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+dKxL( €€˜˜‚Q€ ‚’IMLĮM9 @€!€†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 constant1xLņM1£’’’’’’’’’’’’ņMpķ±ĮMßN< F€c€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ€ ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ņM O( €€˜˜‚Q€ ‚’ āßN6> 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 te O6ĮMmperaturevalue.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: Op) "€"€†Ų”Q€ ‚’the Main menu.16”1…’’’’’’’’’’’’”õƒé°pŠ‚9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+”µ‚( €€˜˜‚Q€ ‚’@Š‚õƒ9 @€€†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 constant1µ‚&„1•’’’’’’’’’’’’&„Š‡é°õƒ…9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+&„:…( €€˜˜‚Q€ ‚’Ł…P‡= 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::…Š‡) "€"€†Ų”Q€ ‚’the Main menu.1P‡»‡1€’’’’’’’’ ’’’’»‡ Šé°Š‡¤ˆ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+»‡Ļˆ( €€˜˜‚Q€ ‚’;¤ˆ Š8 >€€†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 constant1Ļˆ;Š1’’’’’’’’’ ’’’’;Šœé° Š$‹9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+;ŠO‹( €€˜˜‚Q€ ‚’Ö$‹b= 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:O‹œ) "€"€†Ų”Q€ ‚’the Main menu.1bĶ1 ’’’’’’’’ ’’’’ĶµĮ鰜¶Ž9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĶįŽ( €€˜˜‚Q€ ‚’(ķ¶ŽĮ; 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 + AįŽĮœ4*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 vįŽµĮ* $€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.1ĮęĮ1©’’’’’’’’ ’’’’ęĮ^Äé°µĮĻĀ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ęĮśĀ( €€˜˜‚Q€ ‚’d,ĻĀ^Ä8 >€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.1śĀÄ1 ’’’’’’’’ ’’’’ÄkĘé°^ÄxÅ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ä£Å( €€˜˜‚Q€ ‚’ȘxÅkĘ0 .€1€†Ų”Q€‚€ ‚‚‚’Steam ApproximationsThis section deals with steam approximations, steam table calculationsare available for both saturated and superheated areas.1£ÅœĘ1’’’’’’’’’’’’œĘkÉé°kʅĒ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+œĘ°Ē( €€˜˜‚Q€ ‚’»ƒ…ĒkÉ8 >€€†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°ĒœÉ1ˆ’’’’’’’’’’’’œÉóĢé°kɅŹ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+œÉ°Ź( €€˜˜‚Q€ ‚’ Ģ…Ź¹Ģ= 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:°ŹóĢ) "€"€†Ų”Q€ ‚’the Main menu.1¹Ģ$Ķ1f’’’’’’’’’’’’$ĶTé°óĢ Ī9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+$Ķ8Ī( €€˜˜‚Q€ ‚’Ņ ĪT> 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 St8ĪTóĢeps 1 through 3, click on the Exit button to go back tothe Main menu.18Ī…1§’’’’’’’’’’’’…ūé°Tn9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+…™( €€˜˜‚Q€ ‚’b,nū6 :€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 Properties1™,1W’’’’’’’’’’’’,Ré°ū9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+,@( €€˜˜‚Q€ ‚’ÕR= H€«€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Steam Approximations: Superheated AreaSTEP 1Enter the desired superheated steam temperature value or go with the defaulttemperature value.STEP 2Enter the desired superheated steam pressure value or go with the defaultpressure value.STEP 3Click on the Calculate button to start the calculation of the steamproperties for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1@ƒ1 ’’’’’’’’’’’’ƒ[é°Rl9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ƒ—( €€˜˜‚Q€ ‚’Ĕl[0 .€)€†Ų”Q€‚€ ‚‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot, Brayton,Rankine, Otto, Diesel, Magnetohydrodynamics and Fuel Cell).1—Œ1Ģ’’’’’’’’’’’’Œ' é°[u 9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Œ  ( €€˜˜‚Q€ ‚’‡Nu ' 9 @€€†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  X 1N’’’’’’’’’’’’X ué°' A 9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+X l ( €€˜˜‚Q€ ‚’ ĢA u= 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.1l ¦1A’’’’’’’’’’’’¦@é°u9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¦ŗ( €€˜˜‚Q€ ‚’¹‰@0 .€€†Ų”Q€‚€ ‚‚‚’Power Cycles: Braytoŗ@unThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.1ŗ°@1’’’’’’’’’’’’°@ƒDé°@™A9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+°@ÄA( €€˜˜‚Q€ ‚’Ū™AŚC; 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.©ÄAƒD* $€ž€†Ų”Q€ ‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1ŚC“D1i’’’’’’’’’’’’“DģI鰃DE9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+“DČE( €€˜˜‚Q€ ‚’@EH? L€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Power (Ideal)STEP 1Select the desired specie (working fluid) or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine inlet temperature value or go with the defaulttemperature value.STEP 5Enter the desired turbine inlet pressure value or go with the defaultä«ČEģI9 @€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.1HJ1\’’’’’’’’’’’’JHNé°ģIK9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+J1K( €€˜˜‚Q€ ‚’ŪKEM9 @€·€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Power (Real)This subsection provides analysis of the Brayton cycle for the powergeneration application.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateÕ1KHN. *€«€†Ų”Q€ ‚‚‚‚‚’Assumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1EMyN1Š’’’’’’’’’’’’yNB…é°HNbO9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+yNO( €€˜˜‚Q€ ‚’?bOŲ? L€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Power (Real)OŲHNSTEP 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O„< F€ €†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the compressor isentropic efficiency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor)÷ŲB…2 2€ļ€†Ų”Q€ ‚‚‚‚‚‚‚‚‚’efficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go back to the Main menu.1„s…1’’’’’’’’’’’’s…[‰é°B…\†9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+s…‡†( €€˜˜‚Q€ ‚’9ż\†Ąˆ< 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›q‡†[‰* $€ā€†Ų”Q€ ‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1ĄˆŒ‰1n’’’’’’’’’’’’Œ‰Ɏé°[‰uŠ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Œ‰ Š( €€˜˜‚Q€ ‚’EuŠåŒ? 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« ŠɎ9 @€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.1åŒśŽ1r’’’’’’’’’’’’śŽaĆé°ÉŽ Ą9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.comśŽ ĄɎ+śŽ7Ą( €€˜˜‚Q€ ‚’I  Ą€Ā< F€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Propulsion (Real)This subsection provides analysis of the Brayton cycle for the propulsionapplication.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Thrust, Fuel ConsumptionAssumptions:Isentropic compression and expansion. Ideal combustion, heat transfer.į¶7ĄaĆ+ $€m€†Ų”Q€ ‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1€Ā’Ć1š’’’’’’’’’’’’’ĆQŹé°aĆ{Ä9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+’ƦÄ( €€˜˜‚Q€ ‚’D{ÄźĘ? 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 defaultA¦Ä+É< F€ €†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Enter the compressor isentropic efficiency value or go with the defaultcompressor isentropic efficiency value.STEP 9Enter the turbine isentropic efficiency value or go with the defaultturbine isentropic efficiency value.STEP 10Enter the combustor efficiency value or go with the default combustor&õźĘQŹ1 0€ė€†Ų”Q€ ‚‚‚‚‚‚‚‚’efficiency value.STEP 11Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 12When done with Steps 1 through 11, click on the Exit button to go backto the Main menu.1+É‚Ź1Ś’’’’’’’’’’’’‚Ź+Ķé°QŹkĖ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‚Ź–Ė( €€˜˜‚Q€ ‚’•[kĖ+Ķ: B€·€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: RankineThis subsection provides analysis of the Rankine cycle.Input Values:Turbine Inlet Conditions (Temperature and Pressure), Steam Mass FlowRate, Fuel HHVOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateAssumptions:Isentropic compression and expansion. Ideal combustion and heattransfer.1–Ė\Ķ1’’’’’’’’ ’’’’\Ķé°+ĶEĪ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+\ĶpĪ( €€˜˜‚Q€ ‚’ÓEĪ‹< 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.pĪ‹+ĶSTEP 4Click on the Calculate button to start the calculation of the Rankine cycleoutput values for the chosen input values.ŽbpĪ, (€Ä€†Ų”Q€ ‚‚‚‚’STEP 5When done with Steps 1 through 4, click on the Exit button to go back tothe Main menu.1‹J1Ł’’’’’’’’!’’’’Jņé°39 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+J^( €€˜˜‚Q€‚’*ń3ˆ9 @€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,Exhaust Temperature, Exhaust Pressure, Cycle Efficiency, Working FluidMass Flow Rate, Heat Rate, Power Output, Fuel Consumptionj?^ņ+ &€~€†Ų”Q€ ‚‚‚’Assumptions:Specific heat is constant. Four stroke engine.1ˆ#1µ’’’’’’’’"’’’’#§ é°ņ 9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+#7( €€˜˜‚Q€ ‚’)ź `? L€Õ€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: OttoSTEP 1Select the desired specie (working fluid) or go with the default selection.STEP 2Enter the desired ambient temperature value or go with the defaulttemperature value.STEP 3Enter the desired ambient pressure value or go with the defaultpressure value.STEP 4Enter the desired compression ratio (volumetric) value or go with thedefault compression ratio value.STEP 5Enter the desired combustion temperature value or go with the default!å7 < 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&ō`§ 2 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 Ų 1ļ’’’’’’’’#’’’’Ų –é°§ Į 9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ų ģ ( €€˜˜‚Q€ ‚’2łĮ 9 @€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, FuelxLģ –, (€˜€†Ų”Q€ ‚‚‚‚’ConsumptionAssumptions:Specific heat is constant. Four stroke engine.1Ē1.’’’’’’’’$’’’’ĒmF鰖¼@9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Ē¼@–Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ēē@( €€˜˜‚Q€ ‚’/š¼@C? 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,šē@BE< 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 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+łCmF2 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.1BEžF1“’’’’’’’’%’’’’žFKé°mF‡G9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+žF²G( €€˜˜‚Q€ ‚’2ł‡GäI9 @€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, Outletķ²GK/ ,€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.1äI1K1Å’’’’’’’’&’’’’1K]é°KL9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+1KEL( €€˜˜‚Q€ ‚’4öLyN> 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 ELĶ€< 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 mobiyNĶ€Klity 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.dyN], (€Č€†Ų”Q€ ‚‚‚‚’STEP 11When done with Steps 1 through 10, click on the Exit button to go backto the Main menu.1Ķ€Ž1Ą’’’’’’’’'’’’’Ž„é°]w‚9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ž¢‚( €€˜˜‚Q€ ‚’ßw‚°ƒ/ ,€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¢‚„) "€ˆ€†Ų”Q€ ‚’Oxidant Flow Rate, Fuel Cell Voltage, Power, Fuel Cell Efficiency1°ƒN„1’’’’’’’’(’’’’N„Ŗˆé°„7…9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+N„b…( €€˜˜‚Q€ ‚’ į7…‚‡? 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(öb…Ŗˆ2 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‚‡Ūˆ1’’’’’’’’)’’’’ŪˆĒŠé°Ŗˆĉ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ūˆļ‰( €€˜˜‚Q€ ‚’ŲØĉĒŠ0 .€Q€†Ų”Q€‚€ ‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion, expansion, heat transfer and mixing).1ļ‰ųŠ1Ų’’’’’’’’*’’’’ųŠŸŒé°ĒŠį‹9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ųŠ Œ( €€˜˜‚Q€ ‚’“eį‹ŸŒ. ,€Ź€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1 ŒŠŒ1ņ’’’’’’’’+’’’’ŠŒ‘鰟Œ¹9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ŠŒä( €€˜˜‚Q€ ‚’­p¹‘= 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.1äĀ1Q’’’’’’’’,’’’’ĀsÄ鰑·Ą9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’EngiĀ·Ą‘neering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĀāĄ( €€˜˜‚Q€ ‚’ Ē·ĄėĀB 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 5ˆUāĄsÄ3 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.1ėĀ¤Ä1’’’’’’’’-’’’’¤Ä‡Ēé°sčÅ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¤ÄøÅ( €€˜˜‚Q€ ‚’Ļ‘Å‡Ē> J€#€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1øÅøĒ1W’’’’’’’’.’’’’øĒŽĢ鰇Ē”Č9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+øĒĢČ( €€˜˜‚Q€ ‚’Ę”ČŌŹB R€€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Compression: Isentropic (Real)STEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.STEP 5 ŌĢČŽĢ6 :€©€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass flow rate value or go with the defaultmass flow rate value.STEP 6Enter the desired compressor isentropic efficiency value or go with thedefault compressor isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of compressor outlettemperature and power input values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1ŌŹĶ1Õ’’’’’’’’/’’’’Ķ³Ļé°ŽĢųĶ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ķ#Ī( €€˜˜‚Q€ ‚’SųĶ³Ļ= H€§€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processs:Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid (Specie), Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression1#Ī 1;’’’’’’’’0’’’’ y³Ļ ³Ļé°³Ļõ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+  ( €€˜˜‚Q€ ‚’AžõaC T€ż€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Compression: IsothermalSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired compressor inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired compressor outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired compressor mass value or go with the defaultę y2 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.1aŖ1Ö’’’’’’’’1’’’’ŖOé°y“9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ŗ¾( €€˜˜‚Q€ ‚’‘c“O. ,€Ę€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1¾€1§’’’’’’’’2’’’’€ö é°Oi9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+€”( €€˜˜‚Q€ ‚’Łi¬ ? 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!”ö ) "€B€†Ų”Q€ ‚’Specific heat is not constant.1¬ ' 1Ø’’’’’’’’3’’’’' @é°ö  9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+' ; ( €€˜˜‚Q€ ‚’B } < F€ €†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes: Combustion:Coal/OilSTEP 1Enter the desired fuel (coal or oil) composition or go with the default fuelcomposition.Note: If you decide to change the fuel composition, click on theNormalize button to normalize the fuel composition for you.STEP 2Enter the desired oxidant composition or go with the default oxidantcomposition.Note: If you decide to change the oxidant composition, click on theNormalize button to normalize the oxidant composition for you.%ė; ¢: 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¦} @- (€M€†Ų”Q€ ‚‚‚‚’composition and flame temperature value for the ¢@ö chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1¢²@1š’’’’’’’’4’’’’²@D鰁@›A9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+²@ĘA( €€˜˜‚Q€ ‚’ Ģ›AŃC? 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!ĘAD) "€B€†Ų”Q€ ‚’Specific heat is not constant.1ŃCLD1v’’’’’’’’5’’’’LD‘Jé°D5E9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+LD`E( €€˜˜‚Q€ ‚’7ś5E—G= 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.%ė`E¼I: 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§—G‘J. *€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.1¼IĀJ1Ō’’’’’’’’6’’’’ĀJeL鰑J«K9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĀJÖK( €€˜˜‚Q€ ‚’a«KeL. ,€Ā€†Ų”Q€‚€ ‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1ÖK–L1ķ’’’’’’’’7’’’’–LROé°eLM9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+–LŖM( €€˜˜‚Q€ ‚’ØkMRO= 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.1ŖMƒO1#’’’’’’’’8’’’’ƒOa„é°ROx€9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(ƒOx€RO301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ƒO£€( €€˜˜‚Q€ ‚’ßx€Ā‚@ 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£€a„5 8€Õ€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter the desired turbine/expander mass flow rate value or go with thedefault mass flow rate value.STEP 6Click on the Calculate button to start the calculation of turbine/expanderoutlet temperature and power output values for the chosen input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1Ā‚’„1 ’’’’’’’’9’’’’’„k‡é°a„{…9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+’„¦…( €€˜˜‚Q€ ‚’ň{…k‡= H€€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚’Power CycleComponents/Processes:Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid (Specie), Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1¦…œ‡1»’’’’’’’’:’’’’œ‡&é°k‡…ˆ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+œ‡°ˆ( €€˜˜‚Q€ ‚’Ž…ˆĪŠ@ 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. č°ˆīŒ8 >€Ń€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter the desired turbine/expander mass flow rate value or go with thedefault mass flow rate value.STEP 6Enter the desired turbine/expander isentropic efficiency value or go with the default turbine/expander isentropic efficiency value.STEP 7Click on the Calculate button to start the calculation of turbine/expanderoutlet temperature and power output values for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back to8ĪŠ&( € €†Ų”Q€ ’the Main menu.1īŒW1‘’’’’’’’’;’’’’W·é°&@Ž9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+WkŽ( €€˜˜‚Q€ ‚’L@Ž·; 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 expansion1kŽ Ą1’’’’’’’’<’’’’ ĄhÄ· Ą·é°·õĄ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ Ą Į( €€˜˜‚Q€ ‚’3šõĄSĆC T€į€†Ų”Q€‚ƒ‚ƒ‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power CycleComponents/Processes:Expansion: IsothermalSTEP 1Select the desired specie or go with the default specie.STEP 2Enter the desired turbine inlet temperature value or go with thedefault temperature value.STEP 3Enter the desired turbine inlet pressure value or go with the defaultpressure value.STEP 4Enter the desired turbine outlet pressure value or go with the defaultpressure value.STEP 5Enter the desired turbine mass value or go with the defaultć ĮhÄ2 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.1SĆ™Ä1K’’’’’’’’=’’’’™Ä³Ēé°hÄ‚Å9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+™Ä­Å( €€˜˜‚Q€ ‚’Ė‚ųĒ; 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 losses1­ÅäĒ1Ś’’’’’’’’>’’’’äĒĶé°³ĒĶČ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+äĒųČ( €€˜˜‚Q€ ‚’ßĶČĖ? 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.=ųČSĶ< 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:ĖĶ) "€"€†Ų”Q€ ‚’the Main menu.1SĶ¾Ķ1U’’’’’’’’?’’’’¾Ķ”鰍Ķ§Ī9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+¾ĶŅĪ( €€˜˜‚Q€ ‚’Ɖ§Ī”: 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), OutŅĪ”Ķlet WorkingFluids Mass Flow RateOutput Values:Outlet Working Fluids Temperature -- Mixing TemperatureAssumptions:Ideal mixing -- no losses1ŅĪŅ1W’’’’’’’’@’’’’Ņųé°”»9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ņę( €€˜˜‚Q€ ‚’Ō»ų> 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 theĘęų: B€€†Ų”Q€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’default temperature value.STEP 5Select the desired outlet species (outlet working fluid) or go with the defaultspecies.STEP 6Enter the desired outlet working fluids mass flow rate values or go with the defaultmass flow rate values.STEP 7Click on the Calculate button to start the calculation of mixing outletvalues for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1ų)1¾’’’’’’’’A’’’’)¶é°ų9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+)=( €€˜˜‚Q€ ‚’yK¶. ,€–€†Ų”Q€‚€ ‚‚’Compressible FlowThis section provides analysis of compressible flow.1=ē1P’’’’’’’’B’’’’ē é°¶Š9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ēū( €€˜˜‚Q€ ‚’ ÓŠ 8 >€§€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Velocity of SoundThis section provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1ū7 13’’’’’’’’C’’’’7 9 é°  9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+7 K ( €€˜˜‚Q€ ‚’ī² 9 < 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.1K j 1K’’’’’’’’D’’’’j „é°9 S9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+j ~( €€˜˜‚Q€ ‚’ĪS„8 >€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1~µ1ś’’’’’’’’E’’’’µ4C鰄Ŗ@9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwµŖ@„areP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+µÕ@( €€˜˜‚Q€ ‚’%ēŖ@śB> 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:Õ@4C) "€"€†Ų”Q€ ‚’the Main menu.1śBeC1’’’’’’’’F’’’’eC4Eé°4CND9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+eCyD( €€˜˜‚Q€ ‚’»‹ND4E0 .€€†Ų”Q€‚€ ‚‚‚’Compressible Flow: PropertiesThis subsection provides analysis od stagnation and static properties inthe case of compressible flow.1yDeE1ˆ’’’’’’’’G’’’’eE¼Gé°4ENF9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+eEyF( €€˜˜‚Q€ ‚’C NF¼G8 >€€†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 constant1yFķG1G’’’’’’’’H’’’’ķGLé°¼GÖH9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ķGI( €€˜˜‚Q€ ‚’*źÖH+K@ 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 stagnationŲŖIL. *€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+K4L1|’’’’’’’’I’’’’4LNé°LM9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+4LHM( €€˜˜‚Q€ ‚’7’MN8 >€’€†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 constant1HM°N1õ’’’’’’’’J’’’’°NŌ‚é°N™O9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+°NÄO( €€˜˜‚Q€ ‚’0ņ™O‚> J€å€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚ÄO‚N‚’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¦ÄOŌ‚. *€M€†Ų”Q€ ‚‚‚‚‚’temperature and static pressure values for the chosen input values.STEP 6When done with Steps 1 through 5, click on the Exit button to go back tothe Main menu.1‚ƒ1†’’’’’’’’K’’’’ƒZ…é°Ō‚īƒ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ƒ„( €€˜˜‚Q€ ‚’A īƒZ…8 >€€†Ų”Q€‚€ ‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: NozzleThis subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1„‹…1R’’’’’’’’L’’’’‹…¬‰é°Z…t†9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‹…Ÿ†( €€˜˜‚Q€ ‚’)ėt†Ȉ> 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,䵟†¬‰/ ,€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.1ȈŻ‰1K’’’’’’’’M’’’’Ż‰÷Œé°¬‰ʊ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ż‰ńŠ( €€˜˜‚Q€ ‚’Źʊ÷Œ< 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 constant1ńŠ(1õ’’’’’’’’N’’’’(āĮé°÷ŒŽ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+(<Ž( €€˜˜‚Q€ ‚’ ĢŽRĄ> 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<ŽRĄ÷Œ inlet velocity value or go with the default velocityvalue.STEP 5_<ŽāĮ1 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.1RĄĀ1Š’’’’’’’’O’’’’ĀlÄé°āĮüĀ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ā'Ć( €€˜˜‚Q€ ‚’E üĀlÄ8 >€€†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 constant1'ƝÄ1D’’’’’’’’P’’’’Ä°Čé°lĆÅ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ä±Å( €€˜˜‚Q€ ‚’Ż†ÅĢĒ> 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,䵱ŰČ/ ,€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.1ĢĒįČ1æ’’’’’’’’Q’’’’įČoĖé°°ČŹÉ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+įČõÉ( €€˜˜‚Q€ ‚’zAŹÉoĖ9 @€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 constant1õÉ Ė1s’’’’’’’’R’’’’ Ė•é°oĖ‰Ģ9 @€a€†Ų”Q€€‚€ ‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ Ė“Ģ( €€˜˜‚Q€ ‚’.š‰ĢāĪ> 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“Ģ•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 thrāĪ•oĖust values for the choseninput values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1āĪĘ1]’’’’’’’’S’’’’Ęņ,•ņ) "€€†Ų”Q€ ‚’1Ę’’’’1’’’’’’’’T’’’’’’’’’’’’÷1ī1wT1Helv‹v 9\'~év’øē”ŽTms Rmn‹å]ŹU‹ģƒģSymbolų&öt"&‹&‹WCourierŚ@Ä^ &‰&‰Times New RomanÄ^ &ArialƒFÄ^ƒF&MS Serif‰VöŠFō%Ä^MS Sans SerifŠN÷ƒįTimesN÷ƒį ŠéŠé&‰O ±Helvetica‰W ĄtIÄ^System‹&‹WŃźŃŲ-Courier New‰WƒFėRomanč-@Ä^ &‰G&ĒGScriptėÄ^ +Ą&‰G&Modernt[Ä^&öt&‹Marlett &‰GƒFėArial CEÄ^ &‰G’FArial CYRÄv &‹DŽFArial Greek^ &‰Gė Arial TURFöt[Ä^&öArial Baltic‹G)÷éRPCourier New CE &9u'Courier New CYR+FųCourier New Greek ‹Courier New TUR€’‹Matura MT Script CaPlaybillvöWš²©¾®~ķBookshelf Symbol 1åBookshelf Symbol 2RBookshelf Symbol 3&Haettenschweiler‰FžArial NarrowĘG&ĒGGaramond&ĒG &ĒGMS OutlookFŽšf-<³Ä^Kartika‹Ā& Gt"ŽFžVrindaøPP‰~ŲŒFŚšMS DialogŽFž&‹E& Geneva&ƒ}’u鱋FśNew York‹N‹F ĮtBlackadder ITCFäøBradley Hand ITC+ĄPCopperplate Gothic‰Curlz MTBŽFž&’u‰~ŌEdwardian Script ITEngravers MTwšH-õ³Eras Demi ITCė$Ž0Eras Light ITCFśPVšEurostile˜^Ž0&£Ō Felix TitlingģƒģWVFranklin Gothic BooFranklin Gothic DemFrench Script MTŅt Kristen ITC~š?_uķVLucida Sans&²²Ž0&Matisse ITCU‹ģƒģ&WVPapyrus&öDtŽ0&Perpetua‰^š‹v‹F Rockwell Extra BoldTempus Sans ITC1L“‰VivaldiŽ0&ĒŌ Map SymbolsFīöFt&Garamond Antiqua&ĒGaramond Kursivė’vGaramond Halbfett‹PrimaSans BTT+Ą&‰DAlor CondensedD &‰DAlor&ˆDVšÖŹ§³ŽAlor Narrow CondensAlor Narrow&’tFŽAlor Narrow Wide ŅtAlor Wide0&£Ō ŽFīAmosExtended¶Ä^Ś&’Amosš&µė ‹Ē‹VźėAmosThin3Ųµ+Ą™^_‹å]Bazookaģ WVÄ^ ‹óŒFžBeachCondensed£Ō ė{BeachExtendedt’vWBeachųP+ĄPš’o¦¶»Ō BeachThin&‰ Ąu<ŽFžBeachWidePWš\¹¶Ä^Beeswax’vžVš ĮĶ¶ ĄtCommador Extended^ōCommador WideģƒģWVCommador Extended HCommador Heavyt/&’CommadoruŽFž&’t&’Commador Wide HeavyCuckooPWšĀ3(¶Ä^ų&‹Fuji CondensedWV‹FFuji Extended–· ĄuFuji ŽFž&’t&’t’v Fuji Thin+ĄPš’oµ· ĄFuji Wide’t’v’vGilliam 2Ąu>ŽFž&’tHanzel Condensed%ŽFHanzel Extended\}¶Hanzel0&ĒŌ Ž0&Hanzel ThinU‹ģŽ0&Hanzel Wide &‹W]ŹNinepinŽ0&ĒŌ ŽStandout&9Gu&9W Stylus+Ą]ŹU‹ģŽTechnoHeavy&‹G&‹WTechno‹ģƒģV‹F ‹V‹TubularĮ¹ø Ąt1ŽFž&’Voltage ’v+ĄPPFųVoltage Thin&£Ō =MT Extra U‹ģƒģ WVCentury SchoolbookśMonotype Corsiva éŌMS Mincho“ø Ąuéŗ‹@MS MinchoŽFö‹ń&‹DMS PMinchoŽF &‰&‰W@MS PMincho‹Ł&‹G&‹MS GothicW‹v‹F Ę@MS Gothic Ht+Ž0&MS PGothic&‹EŽF&‰@MS PGothic ė0ŽFMS UI Gothicšh"·ŽF@MS UI Gothic”˜^ŽGulim0&”Ō ^_‹å]Ź@GulimWV’v’v’v’GulimCheŗ‹ų‰Vž Šu Ž@GulimChe‹FžPW’v’vDotum ’v ’v’v‰~ų‰@Dotumš’vś’vųšŲĄ ¹ DotumChe]ŹU‹ģƒģ@DotumChe^1‹ŗ‰Fų‰VśBatang0&ĒŌ +Ą™‹å@Batangvšf-²¹Ä^ų‰^BatangCheW&ĒG’’&‹@BatangChe0&”˜^Ž0Gungsuhƒ’t&’wšØ@Gungsuh’’Ä^ō&‹G&GungsuhChewšH-żŗ’v@GungsuhCheŠF$<õSimSun&ˆGSš Įų» Ą@SimSunSø™RPšä"NSimSunöFtÄ^ō&€O@NSimSun~žu\Ä^ō&?SimHei|K&ƒrB@SimHei&9W4|&9GMingLiU|&ƒs&ƒ@MingLiU’u&9W |&PMingLiU0&ƒ>˜^téó@PMingLiUéńž&€Myriad Condensed WeMyriad Web PšŌg¼Albertus Medium‹VņÄAlbertusŽ0&ĒŌ Albertus Extra BoldITC Avant Garde GotITC Bookman LightˆeITC Bookman Demi+ĄPCG Omegaś&Ē&’wCG Times#»¼é†Ä^ś&ITC Zapf ChancerygClarendonš%ī¼ ŠtŽClarendon CondensedClarendon ExtendedRCoronetu ŅtŽ0&CourierPS^Ž0&£Ō ŠITC Zapf Dingbats&ƒHelvetica Narrow0&ƒLetter GothicŽ0&£Marigold&’wšH-i½’vNew Century SchoolbAntique OlivePč„Antique Olive CompaPalatino+ĄP肾‹ųöFSymbolPSt&’tš°jM¼Univers^ųŒFś&‰ė»ŌUnivers CondensedOCRATTRegulartšØ$2SydnieŽFž&ĒD’’Ä^ų&Futured *&‹^_‹å]ŹVAGRounded BT *ž&öGBazooka Greek&ĒŌ Cuckoo Greek¼¾ ĄuéStandout GreektŽStylus Greek€O&‹GTubular GreekÄ^ü&’wArial Narrow CEFųPArial Narrow CyrĄtArial Narrow GreekųArial Narrow Tur rDArial Narrow BalticBookman Old Style CBookman Old Style GBookman Old Style TBookman Old Style BMS Mincho CE ƒŅ;VMS Mincho CyrVśFīMS Mincho Greek w„öMS Mincho Tur+ĄP‹F MS Mincho Balticŗd@MS Mincho CE^1¾‰F@MS Mincho CyrŌ ė@MS Mincho Greek&‰@MS Mincho Tur‰W+Ą@MS Mincho Baltic&‰MS PMincho CE Ft’MS PMincho CyrƒÄŽMS PMincho Greek]Ź MS PMincho TurƒģV+MS PMincho BalticG@MS PMincho CEBĻ_¾=@MS PMincho CyrŌ ƒ@MS PMincho Greek @MS PMincho Tur”Ō ^@MS PMincho Baltic+MS Gothic CEU‹ģ’vMS Gothic Cyr]ŹU‹MS Gothic Greek&’tMS Gothic Tur%MS Gothic BalticuŽ@MS Gothic CE +ĄėL@MS Gothic Cyrš%™Į@MS Gothic GreekŌ @MS Gothic TurPš%Ē@MS Gothic Balticå]MS PGothic CE‹V‰FMS PGothic Cyrƒ~}MS PGothic Greek^ņ&MS PGothic TurV&;WMS PGothic Baltic +@MS PGothic CE Ąu+@MS PGothic CyrG‰F@MS PGothic Greek‰@MS PGothic Tur^ī&‹@MS PGothic Baltic‰MS UI Gothic CEŚFųMS UI Gothic CyrūšMS UI Gothic Greek’MS UI Gothic Tur0&MS UI Gothic Baltic@MS UI Gothic CE’v@MS UI Gothic Cyr˜^@MS UI Gothic Greek@MS UI Gothic Tur @MS UI Gothic BaltiGulim CEFž’’ė#‹F‹Gulim Cyrė‹D‹T FGulim Greekž|‹Fü‹Gulim TurƎĄ&ĒŌ Gulim Baltic­ĆŽĄ&Ē@Gulim CE¹3²ŽŁ^‹å]Ź@Gulim CyrU‹ģƒģDotumChe Greek0&£Ō DotumChe Tur‹VŽ‰Fč‰DotumChe Baltic’vī‹@DotumChe CE+ÉQš%*@DotumChe CyrFąPø@DotumChe GreekŅu‚‹@DotumChe Turu;Št@DotumChe BalticéwBatang CE‰Vž‹F‹V‰Batang CyrF܋VŽFąBatang GreektéRž‹FBatang TurF܋VŽ‰F‰Batang BalticvšŒŠŽ@Batang CE‰F܉VŽ=’’@Batang Cyr+Ą‰FĪéž@Batang Greek‹F‹V@Batang TurVŅuW’vīR@Batang Baltic”ž;VŅBatangChe CEø™RPšBatangChe Cyrtéjž‹BatangChe GreekŚ‰FüBatangChe TurPš%ŸĀBatangChe Balticvī@BatangChe CEÄ=t@BatangChe Cyr^ &€O@BatangChe Greek_‹å@BatangChe TurG&‹W@BatangChe BalticšGungsuh CE0&ƒ>˜^tGungsuh Cyr酐Ä^Gungsuh GreekFą’’&‹Gungsuh Tur=’’té®Gungsuh Baltic‹W‰F@Gungsuh CEtRP’v’@Gungsuh Cyr+Ą‰Fä‰@Gungsuh Greek%ČČ;@Gungsuh TurY’‹Fā‹V@Gungsuh BalticÄ^&GungsuhChe CE š %ūČGungsuhChe CyrüVžÄGungsuhChe Greek’vņGungsuhChe Turéńž;GungsuhChe Baltic™R@GungsuhChe CEŅtéĒ@GungsuhChe Cyrš’v@GungsuhChe Greek‰F@GungsuhChe Tur~é @GungsuhChe BalticüMyriad Web CEGuP&9Myriad Web Tur‰W ‹FMyriad Web Baltic‹FAlbertus Medium CE&Albertus Medium TurAlbertus Medium BalAlbertus CEvīFęPøAlbertus Turt錿 ŅAlbertus Balticģ’vīITC Bookman Light CITC Bookman Light TITC Bookman Light BITC Bookman Demi CEITC Bookman Demi TuITC Bookman Demi BaCG Omega CE ƒĮ ƒÓSCG Omega Tur™+ĮӋåCG Omega BalticĖ‹š‰CG Times CEŽF&‰u&CG Times Turą!‹ČŽĘ&CG Times Baltic£Ō ^ITC Zapf Chancery CITC Zapf Chancery TITC Zapf Chancery BClarendon CEu]+Ą‰FņClarendon Turd3Œ^ž’Clarendon Baltic| Coronet CE‰Fų‰VśRPCoronet Turśt-ĒFų’’Coronet BalticVž ŠuCourierPS CE‹å]ŹCourierPS Turųš“#`ĢCourierPS BalticFōuHelvetica Narrow CEHelvetica Narrow TuHelvetica Narrow BaLetter Gothic CE3įŹLetter Gothic TurģLetter Gothic BaltiMarigold CEŌ 鏐WMarigold TurF&€LMarigold Baltic&’uAntique Olive CEśšAntique Olive TurŽAntique Olive BaltiPalatino CET  ƒŅPalatino Tur&’tšØ$Palatino BalticŒĒšUnivers CE’tšH-CĖŽUnivers Tur"0&”Ō ^Univers BalticVÄ^‹Univers Condensed CUnivers Condensed TUnivers Condensed BTerminal ƒŅRP+ĄPFixedsys%6Ī‹Nō‹^ö+Small Fonts5ø°;ŽĄ&ƒWST_CzecŽĄ&ĒŌ ė WST_Engl&£Ō ø’’™¹ƒĆWST_Fren&’t’v ’v ’WST_GermĢ‰Fü‰VžŽ 0WST_Ital£Ō Ņ|<ƒ~WST_Spanü&D &T&‹WST_Swed|&9D vTheLearningCompany‹@TerminalU‹ģƒģWVÄ^MS Dialog Light0&ĒMS SystemEx|ōŽFž&News Gothic MTąŽFž&Lucida Handwriting%OCR A Extended÷ß ’tCalisto MT‰D&‰T &9Abadi MT Condensed‰Westminster]ŹU‹ģƒMediascape OSD IconMistralžRPš Į”Ģ ĄuWingdings 2PPPš%›ĻMoney &’wFźPø ™Beesknees ITCt"Ž 0Elephant"0&ĒŌ éEras Bold ITCöGuEras Medium ITCčćEras Ultra ITCéŠĒJuice ITCuéƒ&‹GRockwell‰G&‰W‹Fī‹Snap ITCu&9W tĒFōViner Hand ITCšƒ~ōCroat’w+ĄPPPš%yŠ OCR-A-TT-RegularPø Aritus D= téų ŅuBalmoral D&‹W‰Fö‰Barbedor Tt‹Ć‹VBarbedor T HeavyĄuBauer Bodoni D&’w‹Berkeley Old Style+Caslon No224 ITC T0Compacta D’vü’vų’vöCopperplate T&‹G&‹Dom Casual Dt&’t‹Eurostile T BlackĻ Frankfurter DW  ƒFreestyle Script DžFriz Quadrata ITC TFutura Tč4ö‰Fź‰Vģ=’Futura T Condensed’Futura T Extra BoldFutura T Light&‹W‰Garamond ITC T‹Ć‹VGoudy Handtooled D Handel Gothic D"0&£Kabel ITC TšØ$:ŅÄ^Lubalin Graph ITC TMachine ITC DjŅ Šu)Mariage D&’w&’w+ĄNews Gothic T&9WtNews Gothic T LightNimbus Roman No9 L’Old Towne No536 DčPlaza Swash DØ$ŚŅ ĄVAG Rundschrift D ĄCAC Camelot"0&£Ō Ä^CAC ChampagneÄ^ +Ą&CAC Futura Casual&’CAC Futura Casual BCAC Futura Casual MCAC Krazy Legsу~ CAC Krazy Legs BoldCAC Logo Alternate"CAC Lasko CondensedCAC Leslie’w&’wšCAC Lasko Even WeigCAC MooseģƒģfWV+Ą‰FCAC Norm Heavy²‰F¼‰CAC One SeventyӉFŖCAC Pinafore¤š^+(Ō‰CAC Saxon Bold+ĄP’CAC Shishoni Brush1CAC Valiantv¬’vŖ¹’GoudyOlSt BT^1mŌ‰F²PosterBodoni BTš$.xPosterBodoni It BTĄFutura Md BT.›Ō‰FŌ™Futura XBlk BTuéi’Futura XBlkIt BT®‹^Futura MdCn BT‰VĄ‰NFutura XBlkCn BT‰FĀFutura XBlkCnIt BTvBauerBodni BTšf.#Õ’ParkAvenue BTø’PšfCaslonOpnface BTŌø’DomCasual BT’vÄ’vĀšStaccato222 BTvøW’vExotc350 Lt BT’vÄ’vBalloon XBd BT‹vžé”HandelGothic BT’všLydian BTšź³ÕƒÄø.CommercialScript BTBrush455 BT²’v¤’v¢Amazone BTŽ ։Fž‹FČFreehand591 BT‡’vĄ’Freehand575 BT’vĄ’vBernhardFashion BTPParisian BTt ’v¬’vŖCalligraph421 BTv¢šAdLib BTžt ’v ’vžšHOzHandicraft BTŗšĀ3MisterEarl BTv²šĀ3œSwiss 721 SWA®šĀ3ÆÖArabic Transparent‹Traditional Arabic~ąfdecoru8’vWøPøžąf197 ‰Ž QPš“ ׃Ąe0fdecorøŲ PSšžŽe0fdecoröE t +Ą£Žpe0fdecor ’6Ž ’6Ü Žoe0fdecorņ T׃ÄŽF Times CE&’4‰vüŒFžšTimes Cyr&‰G’vWøTimes Greek ×ƒÄ ŠTimes TurøŚ PSšTimes BalticÜ ŽF &’Helvetica CE Ąu ŽF Helvetica Cyr’tŒĒšHelvetica Greekå]ŹHelvetica TurŽ^ ŽFHelvetica BalticŽ&ŠTahoma CEłĶŽŲ‹Ę^_‹åTahoma CyrVĒF܂fĒFŽTahoma GreekŅ‰Fę‰NčTahoma Turš iŲƒÄ‰Tahoma Balticv š Arial CYR CE&Ę+Ą‰Arial CYR Cyr‰FśFÜArial CYR Greek飒Arial CYR Tur’‹š‹FąArial CYR Baltic~"Arial TUR CE‰vģ‹Fž‰Arial TUR Cyr‹Fī9FArial TUR GreekvÖ’vArial TUR TurŁƒÄ ĄArial TUR BalticęvCourier New CYR CE‰Courier New CYR CyrCourier New CYR GreCourier New CYR TurCourier New CYR BalCourier New TUR CEVCourier New TUR CyrCourier New TUR GreCourier New TUR TurCourier New TUR BalLucida Console CE‹FLucida Console CyrLucida Console GreeLucida Console Tur™Verdana CE+Ā@÷nž_‹åVerdana CyrĒFś(ĒFųVerdana Greek’±‹FVerdana Turś’vų’v’Verdana Balticsż‹š9Arial Black CEéÖ Arial Black CyršZŸ Arial Black GreekƒArial Black Turøš’+Arial Black BalticŁComic Sans MS CEv’Comic Sans MS CyruComic Sans MS GreekComic Sans MS TurčµComic Sans MS BaltiGeorgia CE‹FśĒ=Georgia Cyr^_‹å]ŹGeorgia Greekv ’v šGeorgia Tur ŠuøėGeorgia Baltic’ŪƒÄPalatino Linotype CPalatino Linotype GPalatino Linotype TPalatino Linotype BTrebuchet MS CEŪƒÄTrebuchet MS CyrV+’Trebuchet MS Greek‹Trebuchet MS TurvVTrebuchet MS BalticSylfaen CE ĄtjžČtSylfaen CyrėšŽF&’LSylfaen GreekLx4ŽFSylfaen Tur ŻƒÄėįSylfaen Baltic‹F HDesdemona Greek 9܃Impact CE  ’u+Ą™ėImpact Cyr‹ĆŒĀ^_‹åImpact Greekø<P’vImpact Tur‹š‰Vņø?Impact BalticÄ‹ų‰VGaramond CE‰vš‰~ģGaramond Cyr’vš趞Garamond Greek’vīWšGaramond Tur†ģžPšžGaramond BalticžėŻ®bfe0fdecor‹FžPVøJ/e0fdecorŻƒÄ ėĪ’vņ’€bfe0fdecorīWš¦}܃Īe0fdecorŹU‹ģW‹^bfe0fdecorE’÷ėŃēf93å]ŹU‹ģVÄ^ ‹v    /&;)Lzģ‹N‹F Įu’’UOU’’’’Õ —ƒ†ßˆ¢ŠĖhøv€U‚ ƒօfˆßg®Æ. € ƒl‡ĻŠü ʂxˆ†ŠbE»³ ܄uˆd:Ä7Z ƒc…°‰¶‹—­Z€ ‚߇óˆ‹L‡ Ō †ƒ†؊MKŃ6 · ū9ƒ÷„>ˆš‰¦ b µ 2 _ ƒ d† Xˆ  ŽFö&‰&‰T‹ĘŒĀé +Ą™é’v ’v’v軞‹ų‰Vź Štä‹Fź‰~š‰Fņ‹F ‹V‰Fģ‰Vī‹F‹VŽFö&9Twr&9s &‹&‹T‰F‰Vƒ~u ƒ~ué—+Ąŗ+FģƒŚ‹N‹^ Ūuƒł’v+Ū¹’’;Ór w;Įv‹Ó‹Į+É»+NšƒŪ;Ór w;Įv‹Ó‹Į‰Fü‰VžRP’vī’vģ’vņ’vššü¢-ƒÄ +Ą‹NüNšFž¹t3ÓąFņ+Ą‹NüNģFž¹F$ÓąFī‹Fü‹Vž)FVéZ’’v’v č.‹Ē‹Vź^_‹å]Ź U‹ģ’v’v č’v ’v’vč¢ż‹å]Ź U‹ģƒģVÄ^ƒė‹óŒFž&‹&‹WƒŅ Ņu=š’v ’vžVšHOż3ė ’vžVš 5h2ƒÄ^‹å]ŹU‹ģV‹v ’vV’v ’v’včüż‹š‰V Šu!øPøē*PøPš`3G4ƒÄøPšĪń3ƒÄ‹Ę‹V^‹å]Ź U‹ģƒģWV‹~‹v ŽF&Š*ä+ŅŅRPWŒĄŽF &Š *ķĪŒĀRQ‰~ü‰FžŒĒšüP3ƒÄ Ä^ü&ŠŽĒ&‹Ę‹×^_‹å]ŹU‹ģƒģWVÅ~ ÄvŠ‹Č&*ˆFżĘFž&Š*ĮŅ"ĀĮˆF’ėŠ&*ˆFž Ąu žF’GF€~’uéøē0ŽŲ€~žt} ė€~ż| ~øė+Ąėø’’^_‹å]ŹU‹ģƒģWV‹vŽF&ŠˆF’*ä+ŅRPŒĮDQPQV‹łšü”4ƒÄ Š^’*’ŽĒ&ˆ8‹Ę‹×^_‹å]ŹU‹ģƒģWV‹v‹FPV‹ųšŗ;4ƒÄ‹Č*ä+ŅRPWVDWP‰NžšüH5ƒÄ ŽĒŠFž&ˆ‹ĘŒĀ^_‹å]ŹU‹ģWV‹v ‹~Ž^ ŽF&Š8u €<t!FGėš&Š*’6Š‡ž*Š6:‡ž*u:ßtFGėåøõ5ŽŲ+Ąė"øō4ŽŲŽF &Š*’Š‡ž**äŽF&ŠŠž**ķ+Į^_‹å]ŹU‹ģWV‹v ‹~Ž^ ŽFŠ&8u Ąt FGėń&Š*’6Š‡ž+Š6:‡ž+u:ßtFGėåøe6ŽŲ+Ąė"øė5ŽŲŽF &Š*’Š‡ž+*äŽF&ŠŠž+*ķ+Į^_‹å]ŹU‹ģƒģVÅv‹ĪŒ^śė Š*’6Š‡ž-ˆF€<uļø[6ŽŲ‹Į‹Vś^‹å]ŹU‹ģƒģVÅv‹ĪŒ^śė Š*’6Š‡ž,ˆF€<uļø²6ŽŲ‹Į‹Vś^‹å]Źø@Pø™RPš^1“5ĖU‹ģƒģ$WV‹N‹F Įu+Ąé‹F‰Nč‰Fźø@P’v ’vš^1U7‰Fä‰Vę ŠtŲ‹Vꋹ‰Vāø@Pø™RPš^1i7‹ų‰VŽ Šu’vę’väšĀ3Ž7ė«‹FŽ‰~ō‰Fö‹Ī’v ’v’v’v ’vāQ‹ššü7ƒÄ ‹Fä‹VęŽĘ&‰E&‰Uƒ~t?‹^čŽFź&‹&‹WŒĮÄvō&‰&‰T‹FŽŽĮ&‰?&‰G&‹G& Gu^‹FŽŽFź&‰&‰GėN‹^čŽFź&‹G& Gt‹FŽ&Äw&‰<&‰DÄvō+Ą&‰D&‰‹FŽŽFź&‰&‰G&‹G& u ‹FŽŽFź&‰?&‰Gø^_‹å]ŹU‹ģƒģWV‹vŽF‹ž&‹D& Dt &’u&’ušĀ3q8‹FPVšĀ347^_‹å]ĀU‹ģƒģWV‹^ ‹F Ću+Ąé֐‹~‹F ‰^ä‰Fę‹Ė‰Fö‹FÄvä&9 ߈? @ hA øw ƒx°®±. ²xˆ³b“»µ܄¶déź—ė߇ģ†ƒķ؊"&K#&6 $&ū%&¦ &&µ '&_ (&d† Œ¢Š·Ėā Žv€JÄß²śÆū†Š3ūE^ū³ ‰ūuˆ“ū:Ę1†ń1ŲgŃh· Yhb „h2 Æhƒ ŚhXˆ n«€o«l‡p«üq« ęBß7ēB߃čBß°‰Jß­ J߀XQßóˆYQßLZQß  |9ƒ |>ˆS? NåłօyåłfˆœG¾ ƒĒG¾ĻŠņG¾H¾ʂÄ<€%Z ļ<€%c…=€%Ws%Z‚s% ‚ź©‚%‹Ŗ‚%‡@Ŗ‚%€„ÕE.÷„ŠÕE.š‰$ēdI—ƒ\ŖÓPÕƒ|u&’t &’t ŒĄÄ^&’w&’7ŽĄ&’tš@G:ćŽF&‹\ŃćŃ挡&Ä| &‹ &‹QŽĄ&‰ &‰T&’Dé}‹Ž&‹G @@&;G w&‹w &Ä_&0Ä^&;w wé¹&‹G &+G ‰Fž Ąt'&‹G&‹W‹Č‹ņ&G ‹Ł‹NžV‹ū‹šŽŚŃéó„Éó¤Ä^&ĒG ‹Fž&‰G =’snÄ^&‹G&‹W&9Ww]r&9GsUø’&+G ‹ų+Ņ&‹O&‹w&+O&w;ņwr;Čs&‹&++ĄP&’w&’w&Ä_&’wšą1rćƒÄ=’’u;Šu ė5‹vėb‹vWŽF&‹D&‹T&D RP&Ä\&’wš2<äƒÄ‰Fž=’’u č2žŽ(0&£PTė;ĒtŽ(0&ĒPTøėM‹Ē+ɎF&|&L&D ŽF&‹D &9D wéWž&‹D&‹T&D @@&‰&‰T&‹| ŒĄ&Ä\&‹ ŽĄ&L +Ą^_‹å]ĀU‹ģƒģWV‹~ ‹v‹ßŽF N‹Ęѹѹ‰^üŒFžŲ&‹&‹W‹^ü&‰&‰W ö~‹F PW’v’vVš$F®ä^_‹å]Ā U‹ģƒģWVÄ~&ƒ}u&ĒEė&ĒE ’v’v’vW苿 Ąt HHt7‹vė8‹v‹F‹ŽŃćŃć‹ĻÄ~ &‰ &‰A‰vžFWÄ^&’w&’7’vžšhE&åėø’’ė‹Ę^_‹å]ĀU‹ģƒģWV‹v öt{‹~‹FŽF&ĉ^ųŒFś&’w&’7’v ’v ’^ ĄtQ’v’v’vś’vųčųü Ąt HtHt8ė0’vWÄ^&’w&’7Vš$F†åė‰vžN’vWÄ^&’w&’7’vžč“ž öu‘ė+Ąėø^_‹å]ĀU‹ģWV‹vŽF&ƒ¼Ötk&’“Ö&’“Ō&’“Ņ&ĜĪ&’wš`3—įƒÄ‹ųƒ’’učüŽ(0&£PT+Ąė;Ž^9¼ÖtøčŪŽĄ&ĒPT +Ą¹莣ė‹„Ö+ŅĜĪ&G&W‰”ÖøėŽ^_‹å]ĀU‹ģƒģWVƒn Ä^ &‹‰Füƒ~üteøÄ^&+‡Ö+FüÉ#ĮFü‰Fž Ąt3&‹·Ö&ğŅ‹F ‹V ‹NžQ8‹šŽŚŃéó„Éó¤YÄ^&ÖN )Nüƒ~üt„’v’včūž Ąu˜ėø^_‹å]ŹU‹ģƒģWV‹v‹F Ęt(ŽF&‹„@&‹”B‹ų‰VžVš¦ žęƒÄ‹Nž‹÷‰N ĻuŲ^_‹å]ĀU‹ģWVÄv&ƒ|uQ&‹D& Dt&’t&’tŒĒ蘒ŽĒ+Ą&‰D&‰DŽF&‹D & D tI&’t &’t ŒĒš¦ )ēƒÄŽĒ+Ą&‰D &‰D ė)&‹D& Dt&’t&’tŒĒš¦ iēƒÄŽĒ+Ą&‰D&‰D^_‹å]ĀU‹ģV‹vŽF+Ą&‰D&‰D&ƒ|’ugøZP+ĄPPš>L™ēƒÄŽF&‰&‰T‹Ā& u Ž(0&ĒPT