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df = -(p(i+1,1)+p(i,1))/2 * (y(i+1,1)-y(i,1))
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        SUMX=0.
        SUMY=0.

        DO I=2,MX
          DX = 0.5*SQRT((X(I+1,1)-X(I-1,1))**2+(Y(I+1,1)-Y(I-1,1))**2)
          UXI=0.5*(U(I+1,1)-U(I-1,1))
          VXI=0.5*(V(I+1,1)-V(I-1,1))
         UETA=0.5*(U(I,2)-UB1J(I))
         VETA=0.5*(V(I,2)-VB1J(I))
c         UB1J(I),VB1JʪÂÎÆâ²¾ÁÛή®
         YETA=YE(I,1)
          YXI=YX(I,1)
         XETA=XE(I,1)
          XXI=XX(I,1)
         AJAC=AJ(I,1)

        PXX=(-P(I,J)+2.*(YETA*UXI-YXI*UETA)/AJAC*REI)*HX(I,1)
        PYX=((XETA*UXI-XXI*UETA)+(YETA*VXI-YXI*VETA))/AJAC*REI*HY(I,1)
        PXY=((XETA*UXI-XXI*UETA)+(YETA*VXI-YXI*VETA))/AJAC*REI*HX(I,1)
        PYY=(-P(I,J)+2.*(XXI*VETA+XETA*VXI)/AJAC*REI)*HY(I,1)
c       n(HX(I,1),HY(i,2))¢ªË¡Àþ¥Ù¥¯¥È¥ë

        SUMX = SUMX + (PXX+PYX)*DX
        SUMY = SUMY + (PXY+PYY)*DX

        END DO


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¦Æ=(dv/d¦Ç¡¦d¦Ç/dx) - (du/d¦Ç¡¦d¦Ç/dy)
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c     *** surface vorticity(dvdx-dudy) ***
c
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        ve=.5d0*(-3.d0*v(i,1)+4.d0*v(i,2)-v(i,3))

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c     *** surface vorticity(dvdx-dudy) ***
c
        ue=.5d0*(-3.d0*u(i,1)+4.d0*u(i,2)-u(i,3))
        ve=.5d0*(-3.d0*v(i,1)+4.d0*v(i,2)-v(i,3))

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         fd =0.d0
         fl =0.d0
c
      do 110 i=1,nxm1
c
        dx=xx(i,1)¡¡! dx/d¦Î
        dy=yx(i,1)  ! dy/d¦Î
c
        dp=p(i,1)
c
c     *** surface vorticity(dvdx-dudy) ***
c
        ue=.5d0*(-3.d0*u(i,1)+4.d0*u(i,2)-u(i,3))
        ve=.5d0*(-3.d0*v(i,1)+4.d0*v(i,2)-v(i,3))
c
        zeta=(-ve*yx(i,1)+ue*xx(i,1))*yaci(i,1)
c
        fd =fd -2.d0*dp*dy-2.d0*rei*zeta*dx
        fl =fl -2.d0*dp*dx-2.d0*rei*zeta*dy
c
  110 continue
c

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