?_o’’’’"s_Vl`LGas Dynamics ... - TutorialEngineering Software (c) 1996/&;)z460&Ē˜^‹F ’’Æ’’’’|CONTEXTój|CTXOMAP¹b|FONT.|SYSTEM|TOPICž|TTLBTREEÄbgsuh“UGungsuhChe-#@Gun“[+›F[+’’hoĒB ’’’’eĒB V@S€†Ų”QøUNSim-#ŗ[+ĀR[+’’d!ĒB„’’’’ŖeĒBSi-#?[+GG[+’’īnĒBŒ’’’’ĪfĒBU-#U@[+HN[+’’oĒB©’’’’fĒB¾ gLiU€†Ų”Qæ_@PMingLiUĄbMyriad Conde ed WeĮ-##Ī[+ÖP[+’’ŚpĒBˆ’’’’$iĒB“iēb-#1RC[+-#’’°p×[+ßE[+’’ŅlĒBē’’’’šhĒB[+-#dctlÅ [+ĶL[+’’$pĒB’’’’ŽfĒBin ware€†Ų”Q’’’’’’’’#’’’’’’’’’’’’†Ų Ź-#esh[+pF[+’’mĒBč’’’’ŗ8lĒBĢ-#endo|[+-#’’.mī[+öG[+’’°sĒBS’’’’”hĒB[+-#’’öoI [+QL[+’’ÖmĒBk’’’’öhĒB_nowidctlparcs16asuper#Engineering Software%Lett’’’’’’’’@’’’’’’’’’’’’ [+ ’’VqB-#’’’’Ē [+ĻL[+’’nĒBl’’’’’ € ‰€ ‚’Program DescriptionClaim SheetHow to Use the ProgramLimited WarrantySuggestion/Evaluation FormLicense AgreementPropertiesTemperature - Pressure\+i 1 2€V€€ƒƒćŒ€ ‰€ ‚’Running - Temperature - PressureM±Z2 4€6€°˜€ƒć? € ‰€ ‚’Enthalpy - PressureY( ³1 2€P€€ ƒƒć·€ ‰€ ‚’Running - Enthalpy - PressureLZ’2 4€4€°˜€ƒć@ € ‰€ ‚’Entropy - PressureX'³W1 2€N€€ƒƒćā€ ‰€ ‚’Running - Entropy - Pressure^’µ? N€>€˜˜ć€‰€‚€ƒć°€ ‰€ ‚’Power CyclesCarnotR!W1 2€B€€ƒƒć²ś€ ‰€ ‚’Running - Carnot CycleAµH2 4€€°˜€ƒć±€ ‰€ ‚’BraytonI‘3 6€,€˜˜€ƒƒćn«€ ‰€ ‚’Power (Ideal)e3Hö2 4€f€€ƒƒƒćœG¾€ ‰€ ‚’Running - Brayton Cycle: Power (Ideal)H‘>3 6€*€°˜€ƒƒćo«€ ‰€ ‚’Power (Real)d2ö¢2 4€d€€ ƒƒƒćĒG¾€ ‰€ ‚’Running - Brayton Cycle: Power (Real)J>ģ0 0€4€°˜€ ƒƒćp«‰€ ‚’Propulsion (Ideal)j8¢V2 4€p€€ ƒƒƒćņG¾€ ‰€ ‚’Running - Brayton Cycle: Propulsion (Ideal)IģŸ0 0€2€°˜€ ƒƒćq«‰€ ‚’Propulsion (Real)i7V2 4€n€€ ƒƒƒćH¾€ ‰€ ‚’Running - Brayton Cycle: Propulsion (Real)ŸQŸ§N l€¢€˜˜ć€‰€‚€ƒćé€ ‰€ ‚€ ƒƒćęB߉€ ‚’Power Cycle Components/ProcessesCompressionIsentropic (Ideal)h6 2 4€l€€ ƒƒƒćÄ<€%€ ‰€ ‚’Running - Compression: Isentropic (Ideal)I§X 0 0€2€°˜€ ƒƒćēB߉€ ‚’Isentropic (Real)g5 æ 2 4€j€€ ƒƒƒćļ<€%€ ‰€ ‚’Running - Compression: Isentropic (Real)BX  0 0€$€°˜€ ƒƒćčB߉€ ‚’Isothermal`.æ a 2 4€\€€ ƒƒƒć=€%€ ‰€ ‚’Running - Compression: Isothermal@ ” / .€"€°˜€ ƒćź‰€ ‚’Combustion@a į 0 0€ €˜˜€ ƒƒćJ߉€ ‚’Coal/Oil]+” > 2 4€V€€ ƒƒƒćWs%€ ‰€ ‚’Running - Combustion: Coal/Oil; į y 0 0€€°˜€ ƒƒć J߉€ ‚’GasX&> Ń 2 4€L€€ ƒƒƒć‚s%€ ‰€ ‚’Running - Combustion: Gas?y  / .€ €°˜€ ƒćė‰€ ‚’ExpansionJŃ Z 0 0€4€˜˜€ ƒƒćXQ߉€ ‚’Isentropic (Ideal)f4 Ą 2 4€h€€ ƒƒƒćź©‚%€ ‰€ ‚’Running - Expansion: Isentropic (Ideal)IZ 0 0€2€°˜€ ƒƒćYQ߉€ ‚’Isentropic (Real)e3Ą n 2 4€f€€ ƒƒƒćŖ‚%€ ‰€ ‚’Running - Expansion: Isentropic (Real)B ° 0 0€$€°˜€ ƒƒćZQ߉€ ‚’Isothermal^,n 2 4€X€€ ƒƒƒć@Ŗ‚%€ ‰€ ‚’Running - Expansion: Isothermalj.° x< H€\€˜˜ć€‰€‚€ ƒć"&‰€ ‚’Compressible FlowVelocity of SoundW&Ļ1 2€L€€ ƒƒćŲg€ ‰€ ‚’Running - Velocity of SoundAx/ .€$€°˜€ ƒć#&‰€ ‚’Mach NumberQ Ļa1 2€@€€ ƒƒćh€ ‰€ ‚’Running - Mach Number@”/ .€"€°˜€ ƒć$&‰€ ‚’PropertiesBa @0 0€$€˜˜€ ƒƒć |‰€ ‚’Stagnation” @ ]+”i@2 4€V€€ ƒƒƒć„ÕE.€ ‰€ ‚’Running - Stagnation Properties> @§@0 0€€°˜€ ƒƒć |‰€ ‚’StaticY'i@A2 4€N€€ ƒƒƒćŠÕE.€ ‰€ ‚’Running - Static Properties< §@»BKC/ .€€°˜€ ƒć'&‰€ ‚’DiffuserL C—C3 6€2€˜˜€ƒƒć“‘€ ‰€ ‚’Diffuser (Ideal)X&KCļC2 4€L€€ƒƒƒć^yI.€ ‰€ ‚’Running - Diffuser (Ideal)K—C:D3 6€0€˜˜€ƒƒćµ‘€ ‰€ ‚’Diffuser (Real)W%ļC‘D2 4€J€€ƒƒƒć‰yI.€ ‰€ ‚’Running - Diffuser (Real)< :DĶD/ .€€°˜€ ƒć(&‰€ ‚’ThrustJ‘DE3 6€.€˜˜€ƒƒćķ˜€ ‰€ ‚’Thrust (Ideal)V$ĶDmE2 4€H€€ƒƒƒćńÆJ.€ ‰€ ‚’Running - Thrust (Ideal)IE¶E3 6€,€˜˜€ƒƒćµ‘€ ‰€ ‚’Thrust (Real)U#mE F2 4€F€€ƒƒƒć°J.€ ‰€ ‚’Running - Thrust (Real)1¶E 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:$āŹ…B R€Å€†Ų”Q€‚€ €‚‚‚‚‚‚‚‚‚‚€ ‚€‚’Thermodynamic and Transport PropertiesSingle species 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 species consideration -- fuel mass flow rate ignored and¹¦ƒĖ‡H ^€s€†Ų”Q€‚‚‚‚‚€ €‚‚‚‚‚‚€ ‚€‚‚‚€‚’its impact on the properties of the working fluidBasic equations hold (continuity, momentum and energyequations)Specific heat is constantPower Cycle Components/ProcessesSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constantCompressible FlowSingle species considerationBasic equations hold (continuity, momentum and energyequations)Specific heat is constant1Ź…ü‡19’’’’’’’’’’’’ü‡‹é°Ė‡åˆ9 @€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‡‰( €€˜˜‚Q€ ‚’ōŗ刋: B€u€†Ų”Q€‚€‚€ €‚‚‚‚‚‚’How to Use the ProgramIn each section, subsection of the Energy Conversion program, theuser needs to change one or more input 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.1‰5‹1Y’’’’’’’’’’’’5‹iĮé°‹Œ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+5‹IŒ( €€˜˜‚Q€ ‚’7õŒ€ŽB R€ė€†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 thisCóIŒĻĄP n€ē€†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 limi€ŽĻĄ‹ted 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, thenšm€ŽiĮ- *€Ś€†Ų”Q€ €‚‚’Engineering Software shall have no responsibility to replace themedium under the terms of this warranty.1ĻĄšĮ1’’’’’’’’’’’’šĮnÅé°iĮƒĀ9 @€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+šĮ®Ā( €€˜˜‚Q€ ‚’LƒĀśĀ- *€>€†Ų”Q€‚€‚’Suggestion/Evaluation FormÜ®ĀÄ8 >€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.engineering-4e.com‘]śĀŸÄ4 8€ŗ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’Name:Title:Company/Organization:Street Address:City:State:Zip:Phone:FAX:E-Mail:8Ä×Ä) "€€ †Ų”Q€ ‚’Gas Dynamics—ZŸÄnÅ= J€“€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Quality:Usefulness:Possible areas of improvement:Other suggestions:1×ğÅ1k’’’’’’’’’’’’ŸÅŁŹé°nňĘ9 @€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+ŸÅ³Ę( €€˜˜‚Q€ ‚’!ŻˆĘŌČD V€»€†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 afteryour acceptance of this license. Your rights and obligations withrespect to the 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, andŃ³ĘŁŹ4 6€£€†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 software1ŌČ Ė1±’’’’’’’’’’’’ ĖŠĪé°ŁŹóĖ9 @€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+ ĖĢ( €€˜˜‚Q€ ‚’ßóĖ3Ī6 :€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.ĢŠĪ) "€\€†Ų”Q€‚’steam table calculations are not available.13Ī»Ī1]’’’’’’’’’’’’»Ī&鰊Ī¤Ļ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+»ĪĻĻ( €€˜˜‚Q€ ‚’K¤Ļ&9 @€%€†Ų”Q€‚€‚‚‚‚‚ĻĻ&ŠĪ‚‚‚‚‚‚‚’Properties: Temperature - PressureThis subsection provides physical properties of the selected species forassigned temperature and pressure.Input Values:Species, Temperature, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1ĻĻW1„’’’’’’’’ ’’’’WĖķ±&D< 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+Wo( €€˜˜‚Q€ ‚’"äD‘> J€É€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Properties: Temperature - PressureSTEP 1Select the desired species or go with the default species.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Enter the desired pressure value or go with the default pressure value.STEP 4Click on the Calculate button to start the calculation of the physicalproperties for the chosen input values.STEP 5When done with Steps 1 through 4, click on the Exit button to go back to:oĖ) "€"€†Ų”Q€‚’the Main menu.1‘ü1‡’’’’’’’’ ’’’’üRé°Ėå9 @€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( €€˜˜‚Q€ ‚’B åR9 @€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Properties: Enthalpy - PressureThis subsection provides physical properties of the selected species forassigned enthalpy and pressure.Input Values:Species, Enthalpy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1ƒ1—’’’’’’’’ ’’’’ƒé 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€ ‚’ŪlÆ = H€·€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Properties: Enthalpy - PressureSTEP 1Select the desired species or go with the default species.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:—é ) "€"€†Ų”Q€‚’the Main menu.1Æ  1’’’’’’’’ ’’’’ j é°é  9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ . ( €€˜˜‚Q€ ‚’< j 8 >€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Properties: Entropy - PressureThis subsection provides physical properties of the selected species forassigned entropy and pressure.Input Values:Species Entropy, PressureOutput Values:Physical PropertiesAssumptions:Specific heat is not constant1. › 1&’’’’’’’’ ’’’’›  Aé°j „9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+› Æ( €€˜˜‚Q€ ‚’ׄĻ@= H€Æ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Properties: Entropy - PressureSTEP 1Select the desired species or go with the default speciesSTEP 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 ÆĻ@j 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:Æ A) "€"€†Ų”Q€‚’the Main menu.1Ļ@:A1Ļ’’’’’’’’’’’’:AŲBé° A#B9 @€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+:ANB( €€˜˜‚Q€ ‚’Š\#BŲB. ,€ø€†Ų”Q€‚€‚‚’Power CyclesThis section provides analysis of a few power cycles (Carnot and Brayton).1NB C1Ģ’’’’’’’’’’’’ C¤Eé°ŲBņC9 @€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+ CD( €€˜˜‚Q€ ‚’‡NņC¤E9 @€€†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.1DÕE1N’’’’’’’’’’’’ÕEņHé°¤E¾F9 @€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+ÕEéF( €€˜˜‚Q€ ‚’ Ģ¾FņH= 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.1éF#I1ž’’’’’’’’’’’’#IšJé°ņH J9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+#I7J( €€˜˜‚Q€ ‚’¹‰ JšJ0 .€€†Ų”Q€‚€‚‚‚’Power Cycles: BraytonThis subsection provides analysis of the Brayton cycle for both powergeneration and propulsion applications.17J!K1’’’’’’’’’’’’!KōNé°šJ L9 @€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+!K5L( €€˜˜‚Q€ ‚’Ū LKN; 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.©5LōN* $€ž€†Ų”Q€‚‚’Fuel mass flow rate is ignored when calculating the gas turbine poweroutput. No pressure loss. Specific heat is constant.1KN%O1j’’’’’’’’’’’’%Oi„é°ōN€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.engine%O€ōNering-4e.com+%OE€( €€˜˜‚Q€ ‚’@€…‚? 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«E€i„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.1…‚š„1\’’’’’’’’’’’’š„ňé°i„ƒ…9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+š„®…( €€˜˜‚Q€ ‚’Ūƒ…Ā‡9 @€·€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycles: Brayton: Power (Real)This subsection provides analysis of the Brayton cycle for the powergeneration application.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Compressor InletTemperature, Compressor Inlet Pressure, Turbine Inlet Temperature,Turbine Inlet Pressure, Fuel HHV, Compressor Isentropic Efficiency,Turbine Isentropic Efficiency, Combustor EfficiencyOutput Values:Power Output, Fuel Consumption, Cycle Efficiency, Heat RateÕ®…ň. *€«€†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.1Ā‡öˆ1ģ’’’’’’’’’’’’öˆ±é°Åˆ߉9 @€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+öˆ Š( €€˜˜‚Q€ ‚’=ž߉GŒ? L€ż€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Power (Real)STEP 1Select the desired working fluid or go with the default working fluid.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 ŠˆŽ< 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)÷GŒ±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.1ˆŽ Ą1“’’’’’’’’’’’’ ĄōƱ 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€ ‚’9żõĄYĆ< 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 ĮōĆ* $€ā€†Ų”Q€‚‚’output. Ambient pressure is equal to compressor inlet pressure.No pressure loss. Specific heat is constant.1YĆ%Ä1m’’’’’’’’’’’’%ÄaÉé°ōĆÅ9 @€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+%Ä9Å( €€˜˜‚Q€ ‚’DÅ}Ē? L€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Propulsion (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compressor inlet temperature value or go with thedefault temperature value.STEP 3 Enter 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«9ÅaÉ9 @€W€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’turbine inlet pressure value.STEP 6Enter the desired mass flow rate value or go with the default mass flowrate value.STEP 7Enter the desired fuel HHV value or go with the default fuel HHV value.STEP 8Click on the Calculate button to start the calculation of the Brayton cycleoutput values for the chosen input values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.1}Ē’É1o’’’’’’’’’’’’’ÉŠĶé°aÉ{Ź9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+’ɦŹ( €€˜˜‚Q€ ‚’I {ŹļĢ< 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¶¦ŹŠĶ+ $€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.1ļĢĪ1’’’’’’’’’’’’’ĪĪķ±ŠĶīĪ< 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+ĪĻ( €€˜˜‚Q€ ‚’BīĪg? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycles: Brayton: Propulsion (Real)STEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired compreĻgŠĶssor 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 defaultAĻØ< 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&õgĪ1 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.1Ø’1’’’’’’’’’’’’’Ōé°Īč9 @€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€ ‚’Į‘čŌ0 .€#€†Ų”Q€‚€‚‚‚’Power Cycle Components/ProcessesThis section provides analysis of power cycle components/processes(compression, combustion and expansion).11Ų’’’’’’’’’’’’¬é°Ōī9 @€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€ ‚’“eī¬. ,€Ź€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CompressionThis subsection provides analysis of compression.1Ż1ä’’’’’’’’’’’’Ż é°¬Ę 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+Żń ( €€˜˜‚Q€ ‚’ŸfĘ  9 @€Ķ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Compression: Isentropic (Ideal)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1ń Į 1’’’’’’’’’’’’Į {@鰐 Ŗ 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+Į Õ ( €€˜˜‚Q€ ‚’ĢŖ Ż< F€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Compression: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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.’]Õ {@5 8€»€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter 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 Ż{@ input values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1Ż¬@1’’’’’’’’’’’’¬@Cé°{@•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+¬@ĄA( €€˜˜‚Q€ ‚’Į‡•AC: B€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Compression: Isentropic (Real)This subsection provides analysis of isentropic compression.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, CompressorIsentropic EfficiencyOutput Values:Power Input, Outlet TemperatureAssumptions:Isentropic compression. Specific heat is constant.1ĄA²C1`’’’’’’’’’’’’²CįH鰁C›D9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+²CĘD( €€˜˜‚Q€ ‚’ Ģ›DĻF= H€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Compression: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.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.ŪĘDįH7 <€·€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter 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.1ĻFI1Č’’’’’’’’ ’’’’I©Ké°įHūI9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+I&J( €€˜˜‚Q€ ‚’ƒJūI©K9 @€•€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Compression: IsothermalThis subsection provides analysis of isothermal compression.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal compression1&JŚK1©’’’’’’’’!’’’’ŚK\€é°©KĆL9 @€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+ŚKīL( €€˜˜‚Q€ ‚’ ĢĆLųN> J€™€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Compression: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.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 5X%īL\€3 4€K€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’Enter the desired compressor mass value or go with the defaultmass value.STEP 6Click on the Calculate button to start the calculation of compressor outletvalues for the chosen input values.STEP 7When doneųN\€©K with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1ųN€1Ö’’’’’’’’"’’’’€2‚é°\€v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€ ‚’‘cv2‚. ,€Ę€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: CombustionThis subsection provides analysis of combustion.1”c‚1ŗ’’’’’’’’#’’’’c‚ģ…é°2‚Lƒ9 @€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+c‚wƒ( €€˜˜‚Q€ ‚’+šLƒ¢…; D€į€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/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, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:Complete combustion. No gas dissociation. No heat loss.J!wƒģ…) "€B€†Ų”Q€‚’Specific heat is not constant.1¢…†1ė’’’’’’’’$’’’’†׌é°ģ…‡9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+†1‡( €€˜˜‚Q€ ‚’?‡p‰9 @€ €†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/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.į1‡Š‹9 @€Ć€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Furthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio 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 stoichiometry (1 or > 1) or go with the default stoichiometry value.STEP 6Enter the desired combustion efficiency value or go with theMp‰׌1 0€9€†Ų”Q€‚‚‚‚‚‚‚‚’default combustion efficiency value.STEP 7Click on the Calculate button to start the calculation of combustion gascomposition and flame temperature value for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1Š‹1µ’’’’’’’’%’’’’Ąé°×Œń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€ ‚’āńEĄ; D€Å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/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, Stoichiometry, Combustion EfficiencyOutput Values:Fuel HHV, Fuel Enthalpy, Oxidant Enthalpy, Oxidant to Fuel Ratio, FlameTemperature, Combustion Gas CompositionAssumptions:CoŽEĄ׌mplete combustion. No gas dissociation. No heat loss.J!ŽĄ) "€B€†Ų”Q€‚’Specific heat is not constant.1EĄĄĄ1ę’’’’’’’’&’’’’ĄĄuĒ鰏Ą©Į9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+ĄĄŌĮ( €€˜˜‚Q€ ‚’2ł©ĮÄ9 @€ó€†Ų”Q€€‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/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. ēŌĮ&Ę9 @€Ļ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Furthermore, click on the fuel Normalize button one more time tocalculate the new oxidant to fuel ratio 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 stoichiometry value (1 or > 1) or go with the default stoichiometry value.STEP 6Enter the desired combustion efficiency value or go with theOÄuĒ2 2€;€†Ų”Q€‚‚‚‚‚‚‚‚‚’default combustion efficiency value.STEP 7Click on the Calculate button to start the calculation of combustion gascomposition and flame temperature value for the chosen input values.STEP 8When done with Steps 1 through 7, click on the Exit button to go back tothe Main menu.1&ʦĒ1Ō’’’’’’’’'’’’’¦ĒIÉé°uĒ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+¦ĒŗČ( €€˜˜‚Q€ ‚’aČIÉ. ,€Ā€†Ų”Q€‚€‚‚’Power Cycle Components/Processes: ExpansionThis subsection provides analysis of expansion.1ŗČzÉ1ß’’’’’’’’(’’’’zÉ(Ģé°IÉcŹ9 @€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+zÉŽŹ( €€˜˜‚Q€ ‚’šacŹ(Ģ9 @€Ć€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Expansion: Isentropic (Ideal)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet PressureOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1ŽŹYĢ1š’’’’’’’’)’’’’YĢ0é°(ĢBĶ9 @€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+YĢmĶ( €€˜˜‚Q€ ‚’ÜBĶ…Ļ< F€¹€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Expansion: Isentropic (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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.ŸjmĶ05 8€Õ€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚’STEP 5Enter the desired turbine/expander mass flow rate value or go…Ļ0(Ģ 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…Ļa1ü’’’’’’’’*’’’’a,é°0J9 @€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+au( €€˜˜‚Q€ ‚’·~J,9 @€ż€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processes: Expansion: Isentropic (Real)This subsection provides analysis of isentropic expansion.Input Values:Working Fluid, Working Fluid Mass Flow Rate, InletTemperature, Inlet Pressure, Outlet Pressure, Turbine IsentropicEfficiencyOutput Values:Outlet Temperature, Power OutputAssumptions:Isentropic expansion. Specific heat is constant.1u]1“’’’’’’’’+’’’’]ą é°,F9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+]q( €€˜˜‚Q€ ‚’ŪFˆ< F€·€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Expansion: Isentropic (Real)STEP 1Select the desired working fluid or go with the default working fluid.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. čqØ 8 >€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 to8ˆą ( € €†Ų”Q€’the Main menu.1Ø  1Į’’’’’’’’,’’’’ ” é°ą ś 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€ ‚’|Cś ” 9 @€‡€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Power Cycle Components/Processs: Expansion: IsothermalThis subsection provides analysis of isothermal expansion.Input Values:Working Fluid, Working Fluid Mass, Inlet/Outlet Temperature,Inlet Pressure, Outlet PressureOutput Values:Inlet Volume, Outlet Volume, Outlet DensityAssumptions:Isothermal expansion1% Ņ 1–’’’’’’’’-’’’’Ņ CAé°” » 9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ņ ę ( €€˜˜‚Q€ ‚’<ż» .@? L€ū€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Power Cycle Components/Processes: Expansion: IsothermalSTEP 1Select the desired working fluid or go with the default working fluid.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 mę .@” ass value or go with the defaultćę CA2 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.@tA1¾’’’’’’’’.’’’’tACé°CA]B9 @€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+tAˆB( €€˜˜‚Q€ ‚’yK]BC. ,€–€†Ų”Q€‚€‚‚’Compressible FlowThis section provides analysis of compressible flow.1ˆB2C1S’’’’’’’’/’’’’2CTEé°CD9 @€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+2CFD( €€˜˜‚Q€ ‚’ÖDTE8 >€­€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Velocity of SoundThis subsection provides analysis of velocity of sound.Input Values:Working Fluid, TemperatureOutput Values:Velocity of SoundAssumptions:Specific heat is constant1FD…E12’’’’’’’’0’’’’…E†Hé°TEnF9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+…E™F( €€˜˜‚Q€ ‚’ķ±nF†H< F€c€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Velocity of SoundSTEP 1Select the desired working fluid or go with the default working fluid.STEP 2Enter the desired temperature value or go with the default temperaturevalue.STEP 3Click on the Calculate button to start the calculation of velocity of soundvalue for the chosen input values.STEP 4When done with Steps 1 through 3, click on the Exit button to go back tothe Main menu.1™F·H1K’’’’’’’’1’’’’·HŃJ鰆H I9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+·HĖI( €€˜˜‚Q€ ‚’Ī IŃJ8 >€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Mach NumberThis subsection provides analysis of Mach Number.Input Values:Working Fluid, Temperature, VelocityOutput Values:Mach NumberAssumptions:Specific heat is constant1ĖIK1£’’’’’’’’2’’’’KtNé°ŃJėK9 @€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+KL( €€˜˜‚Q€ ‚’$ęėK:N> J€Ķ€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Mach NumberSTEP 1Select the desired working fluid or go with the default working fluid.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:LtN) "€"€†Ų”Q€‚’the Main menu.1:N„N1L’’’’’’’’3’’’’„N„€ķ±tN’O< 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+„N½O( €€˜˜‚Q€ ‚’»‹’O„€0 .€€†Ų”Q€‚€‚‚‚’Compressible Flow:½O„€tN PropertiesThis subsection provides analysis of stagnation and static properties inthe case of compressible flow.1½Oµ€1ˆ’’’’’’’’4’’’’µ€ ƒ鰄€ž9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+µ€Ɂ( €€˜˜‚Q€ ‚’C ž ƒ8 >€€†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 constant1Ɂ=ƒ1D’’’’’’’’5’’’’=ƒP‡é° ƒ&„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+=ƒQ„( €€˜˜‚Q€ ‚’'é&„x†> J€Ó€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Properties: StagnationSTEP 1Select the desired working fluid or go with the default working fluid.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 stagnationŲŖQ„P‡. *€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.1x†‡1|’’’’’’’’6’’’’‡Ģ‰é°P‡jˆ9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+‡•ˆ( €€˜˜‚Q€ ‚’7’jˆĢ‰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•ˆż‰1L’’’’’’’’7’’’’ż‰Žķ±Ģ‰źŠ< 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+ż‰‹( €€˜˜‚Q€ ‚’/ńźŠD> J€ć€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Properties: StaticSTEP 1Select the desired working fluid or go with the default working fluid.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¦‹Ž. *€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.1DIŽ1Ć’’’’’’’’8’’’’IŽ Ąķ±Ž6< 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+IŽa( €€˜˜‚Q€ ‚’zL6 Ą. ,€˜€†Ų”Q€‚€‚‚’Compressible Flow: NozzleThis subsection provides analysis of nozzle.a ĄŽ1a=Ą1“’’’’’’’’9’’’’=ĄžĀķ± Ą*Į< 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+=ĄUĮ( €€˜˜‚Q€ ‚’I*ĮžĀ8 >€#€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Nozzle (Ideal)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, VelocityOutput Values:Static Temperature, Static Pressure, Mach NumberAssumptions:Specific heat is constant1UĮĻĀ1Y’’’’’’’’:’’’’ĻĀ÷Ę鰞ĀøĆ9 @€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+ĻĀćĆ( €€˜˜‚Q€ ‚’0ņøĆĘ> J€å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Nozzle (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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,äµćĆ÷Ę/ ,€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.1Ę(Ē1ć’’’’’’’’;’’’’(ĒŚÉķ±÷ĘČ< F€c€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ€ ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+(Ē@Č( €€˜˜‚Q€ ‚’š`ČŚÉ: B€Į€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Nozzle (Real)This subsection provides analysis of nozzle.Input Values:Working Fluid, Stagnation Temperature, Stagnation Pressure, Ideal Velocity,Nozzle EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, StaticTemperature, Velocity, Mach NumberAssumptions:Specific heat is constant1@Č Ź1¾’’’’’’’’<’’’’ Ź˜Īé°ŚÉōŹ9 @€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+ ŹĖ( €€˜˜‚Q€ ‚’0ņōŹOĶ> J€å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Nozzle (Real)STEP 1Select the desired working fluid or go with the default working fluid.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 nozzle efficiency value or go with the default nozzleIĖ˜Ī3 4€-€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’efficiency value.STEP 6Click on the Calculate button to start the calculation of Mach number,stagnation temperature and stagnation pressure values for the choseninput values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1OĶÉĪ1Ū’’’’’’’’=’’’’ÉĪš鰘Ī²Ļ9 @€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+ÉĪŻĻ( €€˜˜‚Q€ ‚’Ė²Ļš< F€—€†Ų”ŻĻš˜ĪQ€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’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 Static Pressure, Inlet Mach NumberOutlet Stagnation Temperature, Outlet Stagnation Pressure, OutletVelocity, Outlet Static Temperature, Outlet Static Pressure, Outlet MachNumberAssumptions:Specific heat is constant1ŻĻ!1Ś’’’’’’’’>’’’’!Źé°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+!5( €€˜˜‚Q€ ‚’K  €? L€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Normal ShockSTEP 1Select the desired working fluid or go with the default working fluid.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 5Click on the Calculate button to start the calculation of inlet MachJ5Ź0 .€5€†Ų”Q€‚‚‚‚‚‚‚’number, 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€ū1Ē’’’’’’’’?’’’’ū‘ķ±Źč< 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+ū( €€˜˜‚Q€ ‚’~Pč‘. ,€ €†Ų”Q€‚€‚‚’Compressible Flow: DiffuserThis subsection provides analysis of diffuser.1Ā1’’’’’’’’’@’’’’Ā# 鰑« 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+ĀÖ ( €€˜˜‚Q€ ‚’M« # 8 >€+€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Diffuser (Ideal)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, VelocityOutput Values:Mach Number, Stagnation Temperature, Stagnation PressureAssumptions:Specific heat is constant1Ö T 1K’’’’’’’’A’’’’T né°# = 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+T h ( €€˜˜‚Q€ ‚’"ä= Š> J€É€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Diffuser (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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,äµh n/ ,€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.1ŠŸ1ł’’’’’’’’B’’’’Ÿ@Bé°n”@9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, GŸ”@nermantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+Ÿæ@( €€˜˜‚Q€ ‚’G”@@B: B€€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Diffuser (Real)This subsection provides analysis of diffuser.Input Values:Working Fluid, Static Temperature, Static Pressure, Velocity,Diffuser EfficiencyOutput Values:Mach Number, Ideal Stagnation Temperature, Stagnation Pressure,Stagnation TemperatureAssumptions:Specific heat is constant1æ@qB1“’’’’’’’’C’’’’qBōFé°@BZC9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+qB…C( €€˜˜‚Q€ ‚’&čZC«E> J€Ń€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Diffuser (Real)STEP 1Select the desired working fluid or go with the default working fluid.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 5Enter the desired diffuser efficiency value or go with the default diffuserI…CōF3 4€-€†Ų”Q€‚‚‚‚‚‚‚‚‚‚’efficiency value.STEP 6Click on the Calculate button to start the calculation of Mach number,stagnation temperature and stagnation pressure values for the choseninput values.STEP 7When done with Steps 1 through 6, click on the Exit button to go back tothe Main menu.1«E%G1Ć’’’’’’’’D’’’’%G·Hķ±ōFH< 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+%G=H( €€˜˜‚Q€ ‚’zLH·H. ,€˜€†Ų”Q€‚€‚‚’Compressible Flow: ThrustThis subsection provides analysis of thrust.1=HčH1Ē’’’’’’’’E’’’’čH~Ké°·HŃI9 @€a€†Ų”Q€€‚€‚ƒ‚ƒ‚ƒ‚ƒ‚’Engineering SoftwareP.O. Box 1180, Germantown, MD 20875Phone:(301) 540-3605FAX: (301) 540-3605E-Mail:info@engineering-4e.comWeb Site:http://www.engineering-4e.com+čHüI( €€˜˜‚Q€ ‚’‚IŃI~K9 @€“€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Thrust (Ideal)This 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 constant1üIÆK1c’’’’’’’’F’’’’ÆK§€é°~K˜L9 @€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+ÆKĆL( €€˜˜‚Q€ ‚’1ó˜LōN> J€ē€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Thrust (Ideal)STEP 1Select the desired working fluid or go with the default working fluid.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§pĆL§€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, statiōN§€~Kc 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.1ōNŲ€1’’’’’’’’G’’’’Ų€¾ƒé°§€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€ ‚’Ņ˜Į¾ƒ: B€1€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚’Compressible Flow: Thrust (Real)This subsection provides analysis of thrust.Input Values:Working Fluid, Working Fluid Mass Flow Rate, Stagnation Temperature,Stagnation Pressure, Ideal Velocity, Ambient Pressure, Thrust EfficiencyOutput Values:Ideal Static Temperature, Static Pressure, Ideal Mach Number, Thrust,Static Temperature, Velocity, Mach NumberAssumptions:Specific heat is constant1ģļƒ1‚’’’’’’’’H’’’’ļƒ@‰é°¾ƒŲ„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+ļƒ…( €€˜˜‚Q€ ‚’0ņŲ„3‡> J€å€†Ų”Q€‚€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’Running - Compressible Flow: Thrust (Real)STEP 1Select the desired working fluid or go with the default working fluid.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 Ņ…@‰; D€„€†Ų”Q€‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚‚’rate value.STEP 6Enter the desired ambient pressure value or go with the default ambientpressure value.STEP 7Enter the desired thrust efficiency value or go with the default thrustefficiency value.STEP 8Click on the Calculate button to start the calculation of Mach number,static temperature, static pressure and thrust values for the choseninput values.STEP 9When done with Steps 1 through 8, click on the Exit button to go back tothe Main menu.13‡’’’’1’’’’’’’’I’’’’’’’’’’’’”4˜4˜č3Helv^ &‰G"’Fė Ä^ &Tms Rmn&‹GZ™RP&‹GXÄSymbolPš\<”®Ä^ &‰G"Courier^ ‹F‹V$Times New Roman5Ä^Arial&‹Ńč-@Ä^ &‰GMS SerifŠŠč*ä-@Ä^MS Sans SerifĒG'+TimesÄ^&öt#&‹HelveticaįŃįŁ‰^šŒFSystemė"&ŠŠč*ä‹Courier New‰^šŒFņ&‰Roman^š&öG*@t/Ä^&öScriptŃčÄ^š&‰G+ƒFModern*äÄ^š&‰G+’FėMarlettÄ^&‹GZ™RP&‹Arial CEg*æ&‹G)÷éRPArial CYRG)FŽF &9u'Arial Greek-„‹F+FųArial TURģƒģWVÅv ‹Arial BalticŽ@’š“ƁCourier New CEö€~ģCourier New CYRöWš²Courier New Greek«øCourier New TURWV+ĄCourier New BalticuLucida Console‹Fś‹Lucida Sans UnicodeTimes New Roman CETimes New Roman CYRTimes New Roman GreTimes New Roman TURTimes New Roman BalWingdingsé»&ƒ}’uVerdanaą‰FāĘFę‹N‹Arial Black‹G‰FäėComic Sans MSPšük«GeorgiaFąPššeś³ŽFžFranklin Gothic MedPalatino Linotype’wTahoma&ģ³Ä^Ō&’w&’wTrebuchet MS“šˆeW²WebdingsŌ ‹Ę‹VśėEstrangelo 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