PROGRAM SETAXISYMM4
C=======================================================================
C ********** 4-NODED ELEMENT **********
C------------------- ELEMENT NUMBERING: HORIZONTAL SCAN ----------------
C DATA GENERATING PROGRAM FOR STATIC8QFXAXISYMM-NEW.FOR
C DOMAIN SIZE: TLX BY TLY
C BOUNDARY CONDITIONS
C------------ NORMAL DIRECTION
C ON FACE OF -X: P=P0
C ON FACE OF +X: P=0
C ON FACE OF -Y: V=0
C ON FACE OF +Y: V=0
C------------ TANGENTIAL DIRECTION
C ON FACE OF -X: NATURAL BOUNDARY
C ON FACE OF +X: NATURAL BOUNDARY
C ON FACE OF -Y: NATURAL BOUNDARY
C ON FACE OF +Y: NATURAL BOUNDARY
C NOV. 28, 2012
C EIJI FUKUMORI
C=======================================================================
IMPLICIT REAL*8 ( A-H , O-Z )
PARAMETER ( ND=4, INTEPT=2, MXE=31300, MXN=34410, MXB=21000 )
PARAMETER ( TLX0=0.1D0,TLX1=0.15D0,TLY=0.2D0 )
PARAMETER ( YOUNG=210.D9, POISSON=0.3D0 )
PARAMETER ( NEX=11,NEY=22 )
PARAMETER ( P0=10.D6, ALPHA = 1.D0 )
C=======================================================================
DIMENSION NODEX(MXE,ND), XCOORD(MXN), YCOORD(MXN),
* IBNDFX(MXB),IBNDFY(MXB),BVX(MXB),BVY(MXB),
* IBFORCEX(MXB), IBFORCEY(MXB), BVFORCEX(MXB), BVFORCEY(MXB)
DIMENSION NEUTRAL(MXN)
CHARACTER PROJECT*12,EXFILE*3
LOGICAL YES
C=======================================================================
DATA PROJECT / 'STATIC4.DAT' /
C=======================================================================
C NEX: NEMBER OF ELEMENTS IN RADIAL DIRECTION
C NEY: NEMBER OF ELEMENTS IN VERTICAL DIRECTION
C P0, P1, P2: APPLIED HYDRAULIC PRESSURE
C=======================================================================
THICKNSS = TLX1-TLX0
DX = THICKNSS / NEX
DY = TLY / NEY
NDX = NEX + 1
NDY = NEY + 1
C=======================================================================
WRITE (*,*)' YOUNG MODULUS = ',YOUNG
WRITE (*,*)' POISSON RATIO = ',POISSON
C=======================================================================
C ELEMENT CREATION
NE = 0
DO I = 1 , NEY
DO J = 1 , NEX
NE = NE + 1
IF ( NE .GT. MXE ) STOP 'NE > MXE'
NODEX(NE,1) = (I-1)*NDX + J
NODEX(NE,2) = NODEX(NE,1) + 1
NODEX(NE,3) = NODEX(NE,2) + NDX
NODEX(NE,4) = NODEX(NE,1) + NDX
END DO
END DO
C=======================================================================
C NODAL COORDINATE CREATION
NNODE = 0
DO I = 1 , NDY
DO J = 1 , NDX
NNODE = NNODE + 1
IF ( NNODE .GT. MXN ) STOP 'NNODE > MXN'
XCOORD(NNODE) = THICKNSS * F(DX*(J-1)/THICKNSS,ALPHA) + TLX0
YCOORD(NNODE) = DY*(I-1)
END DO
END DO
C=======================================================================
PI = 4.D0* ATAN (1.D0)
C BOUNDARY CONDITIONS
C==== FIRST KIND
C--------- NAVIER EQUATIONS
NBFX = 0
NBFY = 0
NFORCEX = 0
NFORCEY = 0
C
C------- BOTTOM
DO I = 1 , NDX
NBFY = NBFY + 1
IBNDFY(NBFY) = I
BVY(NBFY) = 0.D0
END DO
C------- TOP
DO I = 1 , NDX
NBFY = NBFY + 1
IBNDFY(NBFY) = I + NEY*NDX
BVY(NBFY) = 0.D0
END DO
C
C==== SECOND KIND
C--------- FACE OF INNER SIDE
DF0 = 2.D0*PI*TLX0*DY*P0
C------ RESET MEMORY FOR NEUMANN TYPE BOUNDARY VALUE
DO I = 1 , NDY
BVFORCEX(I) = 0.D0
END DO
C--------- LOAD DISTRIBUTION FOR PARABOLIC ELEMENT UNDER UNIFORM LOAD
WEIGHT = 1.D0/2.D0
DO I = 1 , NEY
NODE = (I-1)*NDX + 1
NFORCEX = (I-1) + 1
IBFORCEX(NFORCEX) = NODE
BVFORCEX(NFORCEX) = BVFORCEX(NFORCEX) + WEIGHT*DF0
NODE = NODE + NDX
NFORCEX = I + 1
IBFORCEX(NFORCEX) = NODE
BVFORCEX(NFORCEX) = BVFORCEX(NFORCEX) +WEIGHT*DF0
END DO
C=======================================================================
WRITE (*,*) ' NUMBER OF ELEMENTS (NE) = ',NE
WRITE (*,*) ' NUMBER OF NODAL POINTS (NNODE) = ',NNODE
WRITE (*,*) ' NUMBER OF DIRICHLET R (NBFX) = ',NBFX
WRITE (*,*) ' NUMBER OF DIRICHLET Z (NBFY) = ',NBFY
WRITE (*,*) ' NUMBER OF NEUMANN R (NFORCEX) = ',NFORCEX
WRITE (*,*) ' NUMBER OF NEUMANN Z (NFORCEY) = ',NFORCEY
C=======================================================================
C DATA FILE INQUIRY
EXFILE = 'NEW'
INQUIRE ( FILE = PROJECT, EXIST = YES )
IF ( YES ) EXFILE='OLD'
C=======================================================================
C MAKING DATA FILES
C---------- 'PROJECT'.JNK
IR = 1
C---------- PARAMETERS
OPEN ( IR, FILE=PROJECT, STATUS = EXFILE )
WRITE(1,*) YOUNG , POISSON
C---------- ELEMENTS
C---------- ELEMENTS
WRITE(1,*) NE
DO I = 1 , NE
WRITE (1,*) I, (NODEX(I,J), J = 1 , ND )
END DO
C---------- COORDINATES OF NONAL POINTS
WRITE(1,*) NNODE
DO I = 1 , NNODE
WRITE(1,*) I,XCOORD(I), YCOORD(I)
END DO
C---------- DIRICHLET TYPE BOUNDARY CONDITIONS
WRITE(1,*) NBFX
DO I = 1 , NBFX
WRITE (1,*) IBNDFX(I), BVX(I)
END DO
WRITE(1,*) NBFY
DO I = 1 , NBFY
WRITE (1,*) IBNDFY(I), BVY(I)
END DO
C---------- NUEMANN TYPE BOUNDARY CONDITIONS
WRITE(1,*) NFORCEX
IF ( NFORCEX .GT. 0 ) THEN
DO I = 1 , NFORCEX
WRITE(1,*) IBFORCEX(I), BVFORCEX(I)
END DO
ENDIF
WRITE(1,*) NFORCEY
IF ( NFORCEY .GT. 0 ) THEN
DO I = 1 , NFORCEY
WRITE(1,*) IBFORCEY(I), BVFORCEY(I)
END DO
ENDIF
C---------- FINAL
CLOSE (1)
C---------- ELEMENT DRAWING
OPEN ( 1, FILE='ELEMENT4.DAT', STATUS = 'UNKNOWN')
DO I = 1, NE
DO J = 1, ND
WRITE (1,*) XCOORD(NODEX(I,J)), YCOORD(NODEX(I,J))
END DO
WRITE (1,*) XCOORD(NODEX(I,1)), YCOORD(NODEX(I,1))
WRITE (1,*)
END DO
CLOSE (1)
C=======================================================================
C------ CREATION OF PARAMETER FILE TO BE USED IN INCLUDE STATEMENT
CALL BANDWID ( MXE, ND, NE, NODEX, NBW )
OPEN ( 1, FILE='PARAM.DAT', STATUS='UNKNOWN' )
WRITE (1,*) ' PARAMETER ( ND=',ND,', INTEPT=',INTEPT,' )'
WRITE (1,*) ' PARAMETER ( MXE=',NE,', MXN=',NNODE,
* ', MXB=',MAX0(NBFX,NBFY,NFORCEX,NFORCEY), ', MXW=',NBW, ' )'
CLOSE (1)
STOP 'NORMAL TERMINATION'
END
C
C
FUNCTION F (X, A)
IMPLICIT REAL*8 ( A-H , O-Z )
F = X**A
RETURN
END
C
C
SUBROUTINE BANDWID ( MXE , ND , NE , NODEX , NBW )
DIMENSION NODEX(MXE,ND)
C------- RETURN VALUE: NBW
NBW = 0
DO I = 1 , NE
DO J = 1 , ND-1
DO K = J+1 , ND
NBW = MAX0 ( NBW , IABS(NODEX(I,J)-NODEX(I,K)) )
END DO
END DO
END DO
NBW = NBW + 1
WRITE (*,*) ' HALH BANDWIDTH =', NBW
RETURN
END