╨╧рб▒с>■ :<■ 9 ье┴q` Ё┐DbjbjqPqP .::═ дЄЄЄЄЄЄЄООООЪ│v║║║║║║║║&(((((($)hСОL!Є║║║║║LЄЄ║║mъъъ║:Є║Є║&ъ║&ъъrXTЄЄ╚║оав-№╖ц┼ОЇЪм&Г0│║ ОF ╚╚& Єю8║║ъ║║║║║LL╘║║║│║║║║dj $j ЄЄЄЄЄЄ Please see this note:- Why does my inlet static pressure boundary condition not match the surface goal for static pressure at the inlet? The calculation has finished before the goal has converged (due to the other finishing conditions) or the default goalТs criterion is too high to ensure the calculated goal value matches the boundary condition specified. For very viscous fluids or pipe flow problems with very little pressure drop (dominated by dissipation forces) the universal automatic convergence criteria, which stops the run when certain mathematical events are met unfortunately stops the solver prematurely. The automatic stop built into FloWorks works well for most problems but sometimes does not work well for pressure only boundary conditions. The premature stop of the run seems to get worse with increasing pressure differentials. This issue only seems to occur on geometries where most of the pressure drop is due mostly to the frictional dissipation of the flow, in other words straight pipes. Usually if there is an obstacle in the flow, the pressure drop is dominated by the obstruction, and the automatic stop calculation feature in FloWorks will accurately stop the run at the correct time. The current work around is to turn off the automatic stop calculation feature in FloWorks and continue the stopped run. To turn this feature off please do the following: Open the Calculation Control Options dialog and switch off all finish conditions. Click Solve, Run and select Solve and Continue to continue the run. The run will have to be stopped manually when the Surface Goal for Static Pressure at the Inlet reaches the static pressure boundary condition. PE users can also specify the custom goal criterion. If your Results are Different from Test Data or Estimations If the difference is too big Check your initial data and boundary conditions. Check your mesh settings and the mesh itself. Especially check the Minimum Gap Size (MGS). Check your reference data. May be your model changes due to influence of flow action or temperature stress. May be some physical phenomena can not be calculated. Check total or static pressure should be set on the inlet boundary condition. Were all physical phenomena taken into account? Transient. Surface/Surface radiation. Gravitation. Surface roughness. Maybe setting of the inlet flow parameters profiles would improve the situation. Has your task converged? Check monitor warnings. Are you in transition mode between laminar and turbulent region? Try to use better mesh. Check whether the compared parameter you use as a reference has actually a small relative difference (the difference could be large in value but small percentage wise). Is there flow separation? Note: When comparing test data with calculation results, please, pay your attention to the following topics:Й╚╥qyJLРТ>BD№єф№┌╨┼к┼иЦ┼Ц┼Ц┼ТОhC%ГhPb+#hPb+hPb+OJQJmH nHtHuU5hPb+hPb+B*fH mH nHph q╩ $jtHuhPb+mH nHtHuhPb+OJQJ^Jh╟WOJQJ^JhPb+hi╚CJOJQJ^Jhi╚hi╚CJhaMЦЙf R└k Т╚╔╩╦╠═╬╧╨╤╥+]М╣╘·ї······ЁЁЁЁЁЁЁЁЁЁЁф╒╒╒╒ &Fдdдd[$\$gdPb+дdдd[$\$gdPb+gdPb+gdi╚gdaMЦD¤╘%[й┘ф pКв√д╛─>@BDЁЁЁЁ▌▌▌▌▌╬╬╬╬╬┬│оомgdaMЦ &Fдdдd[$\$gdPb+дdдd[$\$gdPb+ &Fдdдd[$\$gdPb+ &FДдdдd[$\$^ДgdPb+ &Fдdдd[$\$gdPb+╖Ё What were the parameters measured?╖Ё Where were the measuring points?╖Ё Are there additional components between the measuring points and model inlet/outlet? ,1Рh░╨/ ░р=!░"░#Ра$Ра%░░╨░╨Р╨ЖЬH@ё HNormalCJ_HaJmHnHsH tHuZ@2Zi╚ Heading 3дdдd@&[$\$5БCJ\БaJnHtHuDAЄ бDDefault Paragraph FontRiє │RTable NormalЎ4╓ l4╓aЎ(kЇ ┴(No Listb^@ЄbaMЦNormal (Web)дdдd[$\$CJOJQJ^JaJnHtHuF■OFPb+notenameдdдd[$\$nHtHu>■O>Pb+noteдdдd[$\$nHtHu═ ЙfR└kТ╚╔╩╦╠═╬╧╨╤╥+]М╣╘%[й┘ф p К в √ д ╛ ─ ╩╦╠╧Ш0АА(0ААШ0ААШ0ААШ0ААШ0ААШ0ААШ0АА(0АА(0АА(0АА(0АА(0АА(0АА(0АА(0АА(0АА(0АА(0ААШ0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ 0ААШ0ААШ 0ААШ0ААШ0ААШ0ААЙfR└kТ╚+]М╣╘%[й┘ф p К в √ д ╛ ─ ╩╦╠╧K╚0 АЪ@0ААЪ@0ААЪ@0ААЪ@0ААЪ@0ААЪ@0ААKИ0ф·оЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АЪ@0АШ@0АШ@0АШ@0АШ@0ААЪ@0АА 0?D ╘D DКТЕН╥╘╧ "6B ╥ ╘$DKй╩┘у )*┬╔╧33333333333╣╘┘ p в у √ д ─ ╧╥╘╧8Є░░ Ix@ ООdи СP├?Ъ┬(% л(0aЬ_■╨ Д╨ДШ■╞╨^Д╨`ДШ■CJOJQJo(╖ЁАДаДШ■╞а^Да`ДШ■CJOJQJo(╖ЁАДpДШ■╞p^Дp`ДШ■CJOJQJo(╖ЁАД@ДШ■╞@^Д@`ДШ■CJOJQJo(╖ЁАДДШ■╞^Д`ДШ■CJOJQJo(╖ЁАДрДШ■╞р^Др`ДШ■CJOJQJo(╖ЁАД░ДШ■╞░^Д░`ДШ■CJOJQJo(╖ЁАДАДШ■╞А^ДА`ДШ■CJOJQJo(╖ЁАДPДШ■╞P^ДP`ДШ■CJOJQJo(╖ЁД╨ДШ■╞╨^Д╨`ДШ■CJOJQJo(╖ЁАДаДШ■╞а^Да`ДШ■CJOJQJo(╖ЁАДpДШ■╞p^Дp`ДШ■CJOJQJo(╖ЁАД@ДШ■╞@^Д@`ДШ■CJOJQJo(╖ЁАДДШ■╞^Д`ДШ■CJOJQJo(╖ЁАДрДШ■╞р^Др`ДШ■CJOJQJo(╖ЁАД░ДШ■╞░^Д░`ДШ■CJOJQJo(╖ЁАДАДШ■╞А^ДА`ДШ■CJOJQJo(╖ЁАДPДШ■╞P^ДP`ДШ■CJOJQJo(╖ЁД╨ДШ■╞╨^Д╨`ДШ■CJOJQJo(oАДаДШ■╞а^Да`ДШ■CJOJQJo(oАДpДШ■╞p^Дp`ДШ■CJOJQJo(oАД@ДШ■╞@^Д@`ДШ■CJOJQJo(oАДДШ■╞^Д`ДШ■CJOJQJo(oАДрДШ■╞р^Др`ДШ■CJOJQJo(oАД░ДШ■╞░^Д░`ДШ■CJOJQJo(oАДАДШ■╞А^ДА`ДШ■CJOJQJo(oАДPДШ■╞P^ДP`ДШ■CJOJQJo(oД╨ДШ■╞╨^Д╨`ДШ■CJOJQJo(╖ЁАДаДШ■╞а^Да`ДШ■CJOJQJo(oАДpДШ■╞p^Дp`ДШ■CJOJQJo(зЁАД@ДШ■╞@^Д@`ДШ■CJOJQJo(зЁАДДШ■╞^Д`ДШ■CJOJQJo(зЁАДрДШ■╞р^Др`ДШ■CJOJQJo(зЁАД░ДШ■╞░^Д░`ДШ■CJOJQJo(зЁАДАДШ■╞А^ДА`ДШ■CJOJQJo(зЁАДPДШ■╞P^ДP`ДШ■CJOJQJo(зЁIx@ СP├?8Єл(0a !YТ*H╓3хPb+!dA╟WC%ГaMЦ└пЮc╖i╚ @А╥╥╚'╥╥+═`@` Unknown GРЗ: Times New Roman5РАSymbol3&РЗ: ArialCРИ .PMingLiU░e0}f╘Ъ?5Р Зz А Courier New;РАWingdings"qИЁ╨hR\Ыжa\Ыж┬ ┬ йЁа┤┤ББ24╟╟2ГЁHX)Ё ?ф aMЦ▓ Please see this note:-Kapil GaitondeKapil Gaitonde■ рЕЯЄ∙OhлС+'│┘0РРШ╕─▄шЇ , LX dpxАИфPlease see this note:-Kapil GaitondeNormal.dotKapil Gaitonde5Microsoft Office Word@F├#@Шх├╡ц┼@▓V▄╖ц┼┬ ■ ╒═╒Ь.УЧ+,∙о0 hpЬдм┤╝─╠╘ ▄ ф$3DPLM Software Solutions Ltd., Pune╟цPlease see this note:-Title ■ ■ !"#$%&'(■ *+,-./0■ 2345678■ ¤ ;■ ■ ■ Root Entry └FР]2№╖ц┼=АData 1Table ; WordDocument .SummaryInformation( )DocumentSummaryInformation8 1CompObj q ■ ■ └FMicrosoft Office Word Document MSWordDocWord.Document.8Ї9▓q