SUBROUTINE PressureAnnAndOHDistribution !! Record of revisions !! Date Programmer Discription of change !! ------ ------------ ----------------------- !! 1396/07/30 Sheikh Original code !! USE FricPressDropVars USE MudSystemVARIABLES USE PressureDisplayVARIABLES USE GeoElements_FluidModule USE Fluid_Flow_Startup_Vars USE KickVariables USE CMudPropertiesVariables USE TD_WellGeometry USE CReservoirVariables USE MudSystem USE CHOKEVARIABLES USE CChokeManifoldVariables USE VARIABLES USE CError USE , INTRINSIC :: IEEE_ARITHMETIC IMPLICIT NONE INTEGER :: i , j , k , l INTEGER :: ifric REAL :: Fraction KBOP = 0.0 IF (WellHeadOpen .OR. NoGasPocket == 0) THEN !! (mud circulation is normal wellhead may be open or closed) OR (kick is in the well and well head is open) !!!!! Determining flow rate in each section i = AnnulusFirstEl j = OpenholeFirstEl - 1 !!!!!!!!!!!!!!!!!!!!!!!!! flowrates due to external sources like pump and tripping !WRITE (*,*) 'StringFlowRate', StringFlowRate FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate = (ClingingFactor * FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%Area + FlowEl(StringFirstEl)%Area) * DrillStringSpeed * ConvMintoSec * Convft3toUSgal ! flowrate in annulus due to tripping FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate = FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate + REAL(MudVolume_InjectedToBH) * ConvMintoSec / dt ! flowrate in annulus due to pump !WRITE (*,*) 'Drillstring speed (ft/s)' , FlowEl(j)%FlowRate !IF (NoWellToChokeEl > 0) THEN ! flowrate in choke line ! FlowEl(NoHorizontalEl + NoStringEl + NoAnnulusEl + 1 : NoHorizontalEl + NoStringEl + NoAnnulusEl + NoWellToChokeEl)%FlowRate = AnnulusFlowRate + (DeltaVolumePipe * ConvMinToSec / dt) !END IF IF (ShoeFractured) THEN ! reduction of flowrate due to formation fracture and lost circulation !WRITE (*,*) ' SHoe fractured', PressureGauges(5), FlowEl(ShoeFlowElNo)%FlowRate IF (ShoeFlowElNo > AnnulusLastEl) THEN ! shoe is in openhole FlowEl(ShoeFlowElNo : NumbEl)%FlowRate = - QLost FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate = FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate - QLost ELSE ! shoe is in annulus FlowEl(ShoeFlowElNo : OpenholeFirstEl - 1)%FlowRate = FlowEl(ShoeFlowElNo : OpenholeFirstEl - 1)%FlowRate - QLost END IF END IF !!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!! initial guess flowrates for opening BOP or choke line IF (WellHeadWasOpen == .FALSE. .AND. NoGasPocket > 0 .AND. KickIteration == 1) THEN IF (ChokeKroneckerDelta == 1) THEN ! flow on choke line IF (TotalOpenChokeArea < 0.01 * ChokeAreaFullyOpen) THEN WRITE (*,*) 'density , TotalOpenChokeArea' , density, TotalOpenChokeArea TotalOpenChokeArea = 0.01 * ChokeAreaFullyOpen END IF Kchoke = (ChokeDensity / ((2.0 * 89158.0) * (0.26 * 0.61 * TotalOpenChokeArea)**2)) * 4.0 ! *4.d0: seyyed gofte GasPocketFlowInduced%Array(:) = MIN((0.6 / NoGasPocket * SQRT(PressureGauges(2) / Kchoke)) , (0.05 * GasPocketNewVol%Array(:) * ConvFt3toUSgal / 60 / dt)) WRITE (*,*) ' PressureGauges(2) , Kchoke' , PressureGauges(2) , Kchoke WRITE (*,*) 'Initial guess after opening choke =', GasPocketFlowInduced%Array(1) WRITE (*,*) ' valve 49 ', Valve(49)%Status WRITE (*,*) ' valve 47 ', Valve(47)%Status WRITE (*,*) ' valve 26 ', Valve(26)%Status WRITE (*,*) ' valve 30 ', Valve(30)%Status WRITE (*,*) ' valve 34 ', Valve(34)%Status WRITE (*,*) ' valve 63 ', Valve(63)%Status WRITE (*,*) ' valve 28 ', Valve(28)%Status WRITE (*,*) ' valve 33 ', Valve(33)%Status WRITE (*,*) ' valve 62 ', Valve(62)%Status WRITE (*,*) ' valve 36 ', Valve(36)%Status WRITE (*,*) ' valve 38 ', Valve(38)%Status ELSE ! flow through bell nipple k = NoHorizontalEl + NoStringEl + NoAnnulusEl KBOP = FlowEl(AnnulusLastEl)%Density / ((2.0 * 89158.0) * (0.26 * 0.61 * MinimumOpenArea_InBOP)**2) GasPocketFlowInduced%Array(:) = MIN((0.1 / NoGasPocket * SQRT(PressureGauges(6) / KBOP)) , (0.05 * GasPocketNewVol%Array(:) * ConvFt3toUSgal / 60 / dt)) WRITE (*,*) 'PressureGauges(6), KBOP', PressureGauges(6), KBOP WRITE (*,*) 'Initial guess after opening BOP =', GasPocketFlowInduced%Array(1) END IF END IF !!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!! flowrates due to expansion of gas pockets or kick influx !i = AnnulusFirstEl !j = OpenholeFirstEl - 1 IF (NoGasPocket > 0) THEN DO l = 1 , NoGasPocket !GasPocketFlowEl k = GasPocketFlowEl(l , 1) !WRITE (*,*) 'GasPocketFlowEl(l , 1)', l, k, j IF (k == 0) CALL ERRORSTOP('GasPocketFlowEl(l , 1) == 0', l) IF (k >= OpenholeFirstEl) THEN ! gas pocket is in open hole only FlowEl(k : NumbEl)%FlowRate = FlowEl(k : NumbEl)%FlowRate + GasPocketFlowInduced%Array(l) ! openhole elements above pocket FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate = FlowEl(AnnulusFirstEl : OpenholeFirstEl - 1)%FlowRate + GasPocketFlowInduced%Array(l) ! annulus and choke line elements ELSE IF (k < OpenholeFirstEl) THEN ! gas pocket is in annulus ond/or choke line only FlowEl(k : OpenholeFirstEl - 1)%FlowRate = FlowEl(k : OpenholeFirstEl - 1)%FlowRate + GasPocketFlowInduced%Array(l) ! annulus or choke line elements above pocket END IF END DO END IF !IF (ChokeKroneckerDelta == 1 .AND. ABS(FlowEl(i + NoAnnulusEl)%FlowRate / 600.0 - Ann_Saved_MudDischarged_Volume_Final) > 0.05) THEN ! WRITE (*,*) 'Difference between flowrates', FlowEl(i + NoAnnulusEl + 1)%FlowRate / 600.0, Ann_Saved_MudDischarged_Volume_Final !END IF !!!!!!!!!!!!!!!!!!!!!!!!! !!!!! END - Determining flow rate in each section !!!!!!!!!!!!!!!!!!!!!!!!! effect of surge and swab on frictional pressure drop direction DO l = AnnulusFirstEl , OpenholeFirstEl - 1 IF (FlowEl(l)%FlowRate < 0.0) THEN FlowEl(l)%FrictionDirection = -1 IF (FlowEl(l)%FlowRate > -1.0 * PressFlowrateTolerance .AND. ALLOCATED(GasPocketWeight%Array)) FlowEl(l)%FlowRate = - PressFlowrateTolerance ELSE FlowEl(l)%FrictionDirection = 1 IF (FlowEl(l)%FlowRate < PressFlowrateTolerance .AND. ALLOCATED(GasPocketWeight%Array)) FlowEl(l)%FlowRate = PressFlowrateTolerance END IF END DO !!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!! Calculating Back Pressure, in well to pit path back pressure = 0 ! in well to choke manifold path back pressure is equal to pressure before choke not casing pressure IF (ChokeKroneckerDelta == 1) THEN IF (FlowEl(OpenholeFirstEl - 1)%FlowRate < 0.0) THEN WRITE (*,*) ' Negative choke flowrate' FlowEl(OpenholeFirstEl - 1)%FlowRate = MAX((REAL(MudVolume_InjectedToBH) * ConvMintoSec / dt) , 10.0) END IF !Kchoke = ChokeDensity / ((2. * 89158.0) * (0.26 * 0.61 * TotalOpenChokeArea)**2) deltaPchoke = (Kchoke * FlowEl(OpenholeFirstEl - 1)%FlowRate * ABS(FlowEl(OpenholeFirstEl - 1)%FlowRate)) * 1.d0 !WRITE (*,*) '**deltaPchoke , Kchoke, choke flowrate' , deltaPchoke , Kchoke, FlowEl(i)%FlowRate !WRITE (*,*) '**TotalOpenChokeArea , Total Open Choke Area Percent' , TotalOpenChokeArea , TotalOpenChokeArea / 4.0 * ChokeAreaFullyOpen IF (deltaPchoke < 0.d0) deltaPchoke = 0.d0 BackPressure = REAL(deltaPchoke) !WRITE (*,*) ' Choke inlet FlowRate, Density, pressure' , FlowEl(j)%FlowRate, FlowEl(j)%Density, FlowEl(j)%StartPress !WRITE (*,*) ' Choke outlet Density' , FlowEl(i)%Density !WRITE (*,*) ' deltaPchoke , choke flowrate' , deltaPchoke , FlowEl(i)%FlowRate !WRITE (*,*) 'Total Open Choke Area Percent' , TotalOpenChokeArea / 4.0 * ChokeAreaFullyOpen ELSE BackPressure = 0.0 END IF IF (IEEE_IS_NaN(BackPressure)) CALL ErrorStop('NaN in calculating back pressure' , FlowEl(j)%FlowRate) !write(*,*) 'BackPressure=' , BackPressure !!!!!!!!!!!!!!!!!!!!!!!!! when flow passes through choke manifold, solution process may be unstable IF (ChokeKroneckerDelta == 1) THEN ! thus we should stabilize solution IF (TotalOpenChokeArea > 0.5 * ChokeAreaFullyOpen) THEN KickCorrectionUnderRelaxation = 0.6 ELSE IF (TotalOpenChokeArea > 0.1 * ChokeAreaFullyOpen) THEN KickCorrectionUnderRelaxation = 0.5 ELSE ! TotalOpenChokeArea < 0.1 * ChokeAreaFullyOpen KickCorrectionUnderRelaxation = 0.4 END IF ELSE KickCorrectionUnderRelaxation = 0.6 END IF !!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!! calculating frictional pressure drop in annulus, chooke line and open hole elements DO ifric = AnnulusFirstEl , NumbEl CALL FricPressDrop(ifric) !WRITE (*,*) ' element No, FlowRate , Density, FricPressLoss', ifric, FlowEl(ifric)%FlowRate, FlowEl(ifric)%Density, FlowEl(ifric)%FricPressLoss IF (IEEE_IS_NaN(FlowEl(ifric)%FricPressLoss)) THEN WRITE (*,*) 'H, S, A, Ch, O', NoHorizontalEl , NoStringEl , NoAnnulusEl , NoWellToChokeEl , NoOpenHoleEl WRITE (*,*) 'Ann/Op start, end, density, Q, mu, Type' , FlowEl(ifric)%StartX, FlowEl(ifric)%EndX, FlowEl(ifric)%Density, FlowEl(ifric)%FlowRate, FlowEl(ifric)%mueff, FlowEl(ifric)%MaterialType CALL ErrorStop('NaN in calculating pressure drop' , ifric) END IF END DO !IF (ChokeKroneckerDelta == 1) THEN !WRITE (*,*) ' velocity and flowrate', FlowEl(i)%vel, FlowEl(i)%flowrate !WRITE (*,*) ' Theta600, Theta300', FlowEl(i)%Theta600 , FlowEl(i)%Theta300 !WRITE (*,*) ' kIndex , nIndex', FlowEl(i)%kIndex, FlowEl(i)%nIndex !WRITE (*,*) ' last el. mueff, gen. Rey.', i, FlowEl(i)%mueff, FlowEl(i)%GenRe !END IF !!!!!!!!!!!!!!!!!!!!!!!!! Pressure distribution in annulus j = OpenholeFirstEl - 1 FlowEl(OpenholeFirstEl - 1)%EndPress = BackPressure FlowEl(OpenholeFirstEl - 1)%StartPress = FlowEl(OpenholeFirstEl - 1)%EndPress + FlowEl(OpenholeFirstEl - 1)%FricPressLoss + FlowEl(OpenholeFirstEl - 1)%StaticPressDiff !write(*,*) 'FlowEl(j)%StartPress=' ,j, FlowEl(j)%StartPress !write(*,*) 'FlowEl(j)%Length=' ,j, FlowEl(j)%Length, FlowEl(j)%EndX !write(*,*) 'FlowEl(i)%dPdLFric=' ,i, FlowEl(i)%dPdLFric DO l = OpenholeFirstEl - 2 , AnnulusFirstEl , -1 !WRITE (*,*) '123' FlowEl(l)%EndPress = FlowEl(l + 1)%StartPress FlowEl(l)%StartPress = FlowEl(l)%EndPress + FlowEl(l)%FricPressLoss + FlowEl(l)%StaticPressDiff !WRITE(*,*) "ANNULUS: bottom , top Pressure", l , FlowEl(l)%StartPress , FlowEl(l)%EndPress , FlowEl(l)%fricPressLoss !WRITE(*,*) "ANNULUS: Start , End X", FlowEl(l)%StartX , FlowEl(l)%EndX !write(*,*) 'FlowEl(i)%StartPress=' ,i, FlowEl(i)%StartPress !WRITE (*,*) ' FlowEl(i)%GenRe, FlowEl(i)%ReCritLam ' , FlowEl(i)%GenRe , FlowEl(i)%ReCritLam END DO !!!!!!!!!!!!!!!!! Pressure distribution in Open Hole FlowEl(NumbEl)%EndPress = FlowEl(AnnulusFirstEl)%StartPress FlowEl(NumbEl)%StartPress = FlowEl(NumbEl)%EndPress + FlowEl(NumbEl)%FricPressLoss + FlowEl(NumbEl)%StaticPressDiff !WRITE (*,*) 'op top and op down' , FlowEl(NumbEl)%EndPress, FlowEl(j + 1)%StartPress !write(*,*) 'FlowEl(NumbEl)%dPdLFric=' , FlowEl(NumbEl)%dPdLFric !write(*,*) 'FlowEl(NumbEl)%dPdLGrav=' , FlowEl(NumbEl)%dPdLGrav DO l = NumbEl - 1 , OpenholeFirstEl , -1 !WRITE(*,*) ' ope' FlowEl(l)%EndPress = FlowEl(l + 1)%StartPress !IF (FlowEl(i)%FlowRate < 0.0d0) THEN ! FlowEl(i)%StartPress = FlowEl(i)%EndPress - FlowEl(i)%FricPressLoss + FlowEl(i)%StaticPressDiff !ELSE FlowEl(l)%StartPress = FlowEl(l)%EndPress + FlowEl(l)%FricPressLoss + FlowEl(l)%StaticPressDiff !WRITE (*,*) ' Length, static, frictional open' , FlowEl(i)%Length, FlowEl(i)%StaticPressDiff, FlowEl(i)%FricPressLoss !END IF END DO ELSE ! wellhead is closed and kick is in the well !WRITE (*,*) ' well head is closed' k = GasPocketFlowEl(NoGasPocket , 1) !WRITE (*,*) 'k, Pocket Press', k, GasPocketOldPress%Array(NoGasPocket) - StandardPress i = AnnulusFirstEl j = OpenholeFirstEl - 1 FlowEl(k)%StartPress = GasPocketOldPress%Array(NoGasPocket) - StandardPress FlowEl(k)%EndPress = GasPocketOldPress%Array(NoGasPocket) - StandardPress IF (k > OpenholeFirstEl - 1) THEN ! Top pocket StartX is in Open hole !WRITE (*,*) 'here 1' DO l = k - 1 , OpenholeFirstEl , -1 ! below elements in openhole !WRITE (*,*) 'here 1-1' FlowEl(l)%EndPress = FlowEl(l + 1)%StartPress FlowEl(l)%StartPress = FlowEl(l)%EndPress + FlowEl(l)%StaticPressDiff END DO DO l = k + 1 , NumbEl ! Above elements in openhole !WRITE (*,*) 'here 1-2' FlowEl(l)%StartPress = FlowEl(l - 1)%EndPress FlowEl(l)%EndPress = FlowEl(l)%StartPress - FlowEl(l)%StaticPressDiff END DO FlowEl(AnnulusFirstEl)%StartPress = FlowEl(NumbEl)%EndPress FlowEl(AnnulusFirstEl)%EndPress = FlowEl(AnnulusFirstEl)%StartPress - FlowEl(AnnulusFirstEl)%StaticPressDiff DO l = AnnulusFirstEl + 1 , OpenholeFirstEl - 1 FlowEl(l)%StartPress = FlowEl(l - 1)%EndPress FlowEl(l)%EndPress = FlowEl(l)%StartPress - FlowEl(l)%StaticPressDiff END DO ELSE ! Top pocket StartX is in annulus or choke line DO l = k - 1 , AnnulusFirstEl , -1 ! below elements in annnulus FlowEl(l)%EndPress = FlowEl(l + 1)%StartPress FlowEl(l)%StartPress = FlowEl(l)%EndPress + FlowEl(l)%StaticPressDiff END DO DO l = k + 1 , OpenholeFirstEl - 1 ! Above elements in annulus FlowEl(l)%StartPress = FlowEl(l - 1)%EndPress FlowEl(l)%EndPress = FlowEl(l)%StartPress - FlowEl(l)%StaticPressDiff END DO FlowEl(NumbEl)%EndPress = FlowEl(AnnulusFirstEl)%StartPress FlowEl(NumbEl)%StartPress = FlowEl(NumbEl)%EndPress + FlowEl(NumbEl)%StaticPressDiff DO l = NumbEl - 1 , OpenholeFirstEl , -1 FlowEl(l)%EndPress = FlowEl(l + 1)%StartPress FlowEl(l)%StartPress = FlowEl(l)%EndPress + FlowEl(l)%StaticPressDiff END DO END IF ! ! !WRITE (*,*) ' first annulus bottom pressure ' , FlowEl(NoHorizontalEl + NoStringEl + 1)%StartPress ! !WRITE (*,*) ' last OpenHole bottom pressure' , FlowEl(NumbEl)%StartPress ! !WRITE (*,*) ' Gas Pocket pressure' , GasPocket%NewPress END IF !!!!!!!!!!!!!!!!!!!!!! checking pressure for preventing NaN in pressures DO l = OpenholeFirstEl - 1 , AnnulusFirstEl , -1 ! annulus or choke elements !WRITE (*,*) 'start, end' , FlowEl(i)%StartX, FlowEl(i)%EndX IF (IEEE_IS_NaN(FlowEl(l)%EndPress)) THEN WRITE (*,*) 'H, S, A, Ch, O', NoHorizontalEl , NoStringEl , NoAnnulusEl , NoWellToChokeEl , NoOpenHoleEl WRITE (*,*) 'Ann/Ch start, end, density, Q, mu' , FlowEl(l)%StartX, FlowEl(l)%EndX, FlowEl(l)%Density, FlowEl(l)%FlowRate, FlowEl(l)%mueff, FlowEl(l)%MaterialType CALL ERRORSTOP('NaN in EndPress', l) END IF END DO DO l = NumbEl , OpenholeFirstEl - 1 , -1 ! op elements !WRITE (*,*) 'start, end' , FlowEl(i)%StartX, FlowEl(i)%EndX IF (IEEE_IS_NaN(FlowEl(l)%EndPress)) THEN WRITE (*,*) 'H, S, A, Ch, O', NoHorizontalEl , NoStringEl , NoAnnulusEl , NoWellToChokeEl , NoOpenHoleEl WRITE (*,*) 'Op start, end, density, Q, mu' , FlowEl(l)%StartX, FlowEl(l)%EndX, FlowEl(l)%Density, FlowEl(l)%FlowRate, FlowEl(l)%mueff, FlowEl(l)%MaterialType CALL ERRORSTOP('NaN in EndPress', l) END IF END DO !!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!! BottomHolePress = FlowEl(OpenholeFirstEl)%StartPress !DO i = 1 , NoGasPocket ! WRITE (*,*) ' Pocket, Pressure, Vol, Flow Induced, FlowElPress', i, REAL(GasPocketNewPress%Array(i)), REAL(GasPocketNewVol%Array(i)), GasPocketFlowInduced%Array(i), FlowEl(GasPocketFlowEl(i , 1))%StartPress !END DO !WRITE (*,*) ' BottomHolePress =' , BottomHolePress !!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! !IF (ChokeKroneckerDelta == 1) THEN ! WRITE (*,*) ' ChokeLine flowrate' , FlowEl(NoHorizontalEl + NoStringEl + NoAnnulusEl + NoWellToChokeEl)%FlowRate , stringflowrate ! !i = NoHorizontalEl + NoStringEl + NoAnnulusEl ! !j = NoHorizontalEl + NoStringEl + NoAnnulusEl + NoWellToChokeEl ! !WRITE (*,*) ' Well Outlet and Chokeline Outlet Pressure' , FlowEl(i)%EndPress, FlowEl(j)%EndPress !END IF !IF (GasPocket%ElementNo == 0) THEN ! KickUnknownVector(2) = BottomHolePress !!ELSE !! KickUnknownVector(2) = FlowEl(GasPocket%ElementNo)%StartPress !END IF !IF (WellHeadOpen) ! GasPocket%NewPress = KickUnknownVector(2) !END IF !WRITE (*,*) 'Ann End' END SUBROUTINE