
 The notation of the output data: (1,8,15)

^XZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described. The frame lies
    in the same plane.

^U,W^ - displacements of the nodes in the global coordinate system XZ
    respectively. Positive values coincide with the positive directions
    of the axes.

^Ty^ - rotation of the nodes (as a solid body) shearnd axis Y of the
    global coordinate system. The rotation are positive when are
    in anticlockwise direction when looking against axis Y.

^Rx,Rz,My^ - reactions in the fixed nodes in the global coordinate
    system.

^X'Y'Z'^ - axes of local coordinate system.
    The local coordinate system for beam elements has origin in
    the first node J1 of the element. The axis X' points to node J2 of
    the element. The axes Y' and Z' coincide with the principal axes of
    inertia of the crossection. Axes X' and Z' lies on the plane of
    the structure.

^U',W'^  - displacements  of the center of the gravity in local
     coordinate system X'Z'. Positive values coincide with the positive
     directions of the axes.

^T'^ - rotation of the crossection around  axis Y' of local coordinate
    system.

^N,Q,M^ - direct force (N), shear force (Q) and bending moment (M)
    that acts on the crossection of the beam.

^SigmaX(+Z), SigmaX(-Z)^ - value of the maximal direct stress in the
      crossection  due to the normal force N and bending moment M.
      Indexes +Z and -Z point to the sides with +Z and -Z of local
      coordinate Z.

^TauZ^ -  absolute value of the maximal shear stress in the crossection
       due to the shear force Q.

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@1

The notation of the output data: (2)

^XZ^ - axes of the global coordinate system.
    Global coordinate system is a rectangular system in which the nodes
    coordinates are described. The axis Z coincide with the axis of the
    shell.

^U,W^ - displacements of the nodes in the global coordinate system XZ
    respectively. Positive values coincide with the positive directions
    of the axes.

^Ty^ - rotation of the normal to the middle plane of the element,
    crossing the nodes, around axis y of the global coordinate system.
    The rotation are positive when are in anticlockwise direction when
    looking against axis y.

^Rx,Rz,My^ - reactions in the fixed nodes in the global coordinate
    system.

^X'Y'Z'^ - axes of local coordinate system.
    The local coordinate system for element has origin in
    the first node J1 of the element. The axis X' points to node J2 of
    the element and axis Z' points to the axis of the shell. When
    element is curvilinear (sphere,torus) axis X' is tangential to the
    meridian of the shell and axis Z' points to the center of
    curvature. The axis of the shell coincide with the plane X'Z'. Axis
    Y' is tangential to the middle surface of the shell in
    circumferential direction.

^U',W'^ - displacements of the middle surface of the shell in local
    coordinate system X'Z'. Positive values coincide with the positive
    directions of the axes.

^T'^ - rotation of the normal to the middle plane of the shell around
    axis Y' of local coordinate system.

^N,Q,M^ - intensity of direct force (N), shear force (Q) and bending
    moment (M) that acts on the crossection of the shell, perpendicular
    to the axis of the shell. There measure for all is per unit length.

^Mt^-intensity of bending moment in circumferential direction that
    acts on the crossection of the shell, parallel to the axis of the
    shell. The measure of Mt is per unit length.

^SigmaX(+Z), SigmaX(-Z), SigmaY(+Z), SigmaY(-Z)^ - values of the direct
    stresses in  directions X' and Y' respectively. Indexes +Z and -Z
    point to the inner and outer surfaces of the shell.

@2
The notation of the output data:

^XYZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described.

^U,V,W^ - displacements of the nodes in the global coordinate system.
    Positive values coincide with the positive directions of the
    axes.

^Tx,Ty,Tz^ - rotation of the nodes (as a solid body) around axes XYZ
    of the global coordinate system. The rotation are positive when are
    in anticlockwise direction when looking against axes.

^Rx,Ry,Rz,Mx,My,Mz^ - reactions in the fixed nodes in the global
    coordinate system. Positive directions of reactions coinside with
    positive directions of the axes.

^X'Y'Z'^ - axes of local coordinate system.
    The local coordinate system for beam elements has origin in
    the first node J1 of the element. The axis X' points to node J2
    of the element. The axes Y' and Z' coincide with the principal
    axes of inertia of the crossection.

    For plane frame structures (plane frames, plane trusses) axis d Z' lie
    on the plane of the structure.

    For grillages axis Z' is perpendicular to the plane of the
    structure.

    For space frames axis Z' may be in arbitrary orientation in the
    space. The orientation of Z' axis must be given in the input data.

    For trusses orientation of axes Y' and Z' does not influence the
    results.

^N,Qy,Qz,Mx,My,Mz^ - direct force (N), shear forces (Qy and Qz),
    torsion moment (Mx) and bending moments (My and Mz) that acts on
    the crossection of the beam.

^SigmaX^ - absolute value of the maximal direct stress in the
    crossection due to the normal force N and bending moments My and Mz.

^TauMx^ - maximal tangential stress in the crossection due to the torsion
    moment Mx.

^Sigma Eqw ^ - maximal equwivalent stress in the crossection according to
    Von Misses theory due to the SigmaX and TauMx.

^TauQy, TauQz^ - maximal shear stresses in the crossection due to the shear
    forces Qy and Qz respectively.

^N,crit^- normal force that can produce local buckling of the rod element.

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@3

The notation of the output data: (9-11)

^XZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described.

^U,W^ - displacements of the nodes in the global coordinate system.
    Positive values coincide with the positive directions of the
    axes.

^Rx,Rz^ - reactions in the fixed nodes in the global  coordinate system.

^X'Z'^ - axes of local coordinate system.
    Every one element has local coordinate system X'Z' with
    origin in the center of gravity of the element. Axes X' and Z' are
    lying in the plane of the element and are parallel to the axes XZ of
    the global coordinate system.

^SigmaX, SigmaY, SigmaZ, TauXZ^ - stresses in the center of the
    gravity of the element in local coordinate system.

^SigmaI(XZ), SigmaII(XZ)^ - principal stresses in the plane of the
    element.

^TauMax^ - the maximal tangential stress in the plane of the element.

^Sigma (+), Sigma (-)^ - the maximal tension and maximal compression
    in the plane of the element.

^SigmaEq^ - equivalent stress in the center of gravity of the element.
    The appropriate formulae is selectable.

 Tresca Formulae:     SigmaEq = S1-S3

 Von Misses Formulae:
                  _____________________________________________________
 SigmaEq = 0.707 ((S1-S2).(S1-S2) + (S2-S3).(S2-S3) + (S3-S1).(S3-S1))

 Mohr Formulae:      SigmaEq = S1- k.S3

 where S1,S2,S3 are the principal stresses.

 For plastic materials:
         k = Sigma yielding on tension / Sigma yielding on compression

 For brittle materials:
         k = Sigma,B  on tension / Sigma,B on compression

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@4

 The notation of the output data: (13)

^XYZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described. The plate lies in
    the plane XY.

^W^ - displacement of the nodes in the global coordinate system in Z
    direction.Positive values coincide with the positive directions of
    the axes Z.

^Tx,Ty^ - rotation of the normal to the middle plane of the element,
    crossing nodes, around axes X and Y respectively of the global
    coordinate system. The rotation are positive when are in
    anticlockwise direction when looking against axes.

^Rz,Mx,My^ - reactions in the fixed nodes in the global  coordinate
    system.

^X'Y'^ - axes of local coordinate system.
    Every one plate element has local coordinate system X'Y' with
    origin in the center of gravity of the element. Axes X' and Y'
    are lying in the plane of the element and are parallel to the
    axes XY of the global coordinate system.

^SigmaX, SigmaY, TauXY^ - stresses in the center of the gravity of the
    element in local coordinate system. The surface of the plate
    (middle surface, upper or bottom surface) is selectable.

^SigmaI(XY), SigmaII(XY)^ - principal stresses in the  plane of
    the element.

^TauMax^ - the maximal tangential stress in the  plane of the
    element.

^Sigma (+), Sigma (-)^ - the maximal tension and maximal compression
    in the plane of the element.

^SigmaEq^ - equivalent stress in the center of gravity of the element.
    The appropriate formulae is selectable.

 Tresca Formulae:     SigmaEq = S1-S3

 Von Misses Formulae:
                  _____________________________________________________
 SigmaEq = 0.707 ((S1-S2).(S1-S2) + (S2-S3).(S2-S3) + (S3-S1).(S3-S1))

 Mohr Formulae:      SigmaEq = S1- k.S3

 where S1,S2,S3 are the principal stresses.

 For plastic materials:
         k = Sigma yielding on tension / Sigma yielding on compression

 For brittle materials:
         k = Sigma,B  on tension / Sigma,B on compression

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@5

 The notation of the output data:  (14)

^XYZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described.

^U,V,W^ - displacements of the nodes in the global coordinate system.
    Positive values coincide with the positive directions of the
    axes.

^Tx,Ty,Tz^ - rotation of the normal to the middle plane of the
    element, crossing nodes, around axes XYZ of the global coordinate
    system. The rotation are positive when are in anticlockwise
    direction when looking against axes.

^Rx,Ry,Rz,Mx,My,Mz^ - reactions in the fixed nodes in the global
    coordinate system.

^X'Y'Z'^ - axes of local coordinate system.
    Every one shell element has local coordinate system X'Y'Z' with
    origin in the node J1. The axes X'Y' are lying on the middle
    plane of the element. The axis  X' points to node J2 of the
    element. Axis Y' is perpendicular to X'. Axis Z' coincide
    with the  normal to the middle surface. When looking against
    axis Z' the numbering  of nodes is in anticlockwise direction.

^SigmaX, SigmaY, SigmaZ, TauXY^ - stresses in the center of the
    gravity of the element in local coordinate system. The surface
    of the shell (middle surface, inner or outer surface) is
    selectable.

^SigmaI(XY), SigmaII(XY)^ - principal stresses in the plane of
    the element.

^TauMax^ - the maximal tangential stress in the  plane of the
    element.

^Sigma (+), Sigma (-)^ - the maximal tension and maximal compression
    in the plane of the element.

^SigmaEq^ - equivalent stress in the center of gravity of the element.
    The appropriate formulae is selectable.

 Tresca Formulae:     SigmaEq = S1-S3

 Von Misses Formulae:
                  _____________________________________________________
 SigmaEq = 0.707 ((S1-S2).(S1-S2) + (S2-S3).(S2-S3) + (S3-S1).(S3-S1))

 Mohr Formulae:      SigmaEq = S1- k.S3

 where S1,S2,S3 are the principal stresses.

 For plastic materials:
         k = Sigma yielding on tension / Sigma yielding on compression

 For brittle materials:
         k = Sigma,B  on tension / Sigma,B on compression

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@6
 The notation of the output data:  (17)

^XYZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described.

^U,V,W^ - displacements of the nodes in the global coordinate system.
    Positive values coincide with the positive directions of the
    axes.

^Rx,Ry,Rz^ - reactions in the fixed nodes in the global coordinate system.


^SigmaX, SigmaY, SigmaZ, TauXY, TauYZ, TauZX^ - stresses in the center of
    the gravity of the element in local coordinate system. The surface
    of the shell (middle surface, inner or outer surface) is
    selectable.

^Sigma1, Sigma2, Sigma3^ - principal stresses in the plane of the element.

^TauMax^ - the maximal tangential stress in the  plane of the element.

^SigmaEq^ - equivalent stress in the center of gravity of the element.
    The appropriate formulae is selectable.

 Tresca Formulae:     SigmaEq = S1-S3

 Von Misses Formulae:
                  _____________________________________________________
 SigmaEq = 0.707 ((S1-S2).(S1-S2) + (S2-S3).(S2-S3) + (S3-S1).(S3-S1))

 Mohr Formulae:      SigmaEq = S1- k.S3

 where S1,S2,S3 are the principal stresses.

 For plastic materials:
         k = Sigma yielding on tension / Sigma yielding on compression

 For brittle materials:
         k = Sigma,B  on tension / Sigma,B on compression

^Error evaluation^ - the equilibrium of the structure for all load
    cases is checked. The absolute error is the total sum of forces
    along given axis, including external loading and reactions.
    Theoretically this sum must be zero but practically depending of
    the size of the problem solved owing to the errors of rounding
    during computations it can be different from zero.
    Because the reactions of the structure are computed on the base of
    results for displacements it is proposed that if the total
    equilibrium is satisfied the results are acceptable.
    In case the error is too big the possible reason may be bad geometry
    of the structure.
@7
The notation of the output data: (16)

^XZ^ - axes of the global coordinate system.
    Global coordinate system is arbitrary chosen rectangular system
    in which the nodes coordinates are described.

^TauXY, TauXZ^ - shear stresses in the center of gravity of the element.

^TauMax^ - the maximal tangential stress in the center of gravity of
    the element.
@8