------------------------------F06 Info------------------------------

In order for a table to be supported, it must read AND write ALL fields.
Important calculated parameters are nice, but not required.

*** Not done....

#----------------------------------------------------------------------------


----OEF - forces----
Finite Element Temperature Gradients And Fluxes

----OQG - constraint forces----
Forces Of Single-Point Constraint				done
Forces Of Multi-Point  Constraint				done


----OES - stress/strain----
Stresses In Bar Elements(CBAR)					done
Stresses In Rod Elements(CROD)					done

Stresses In Triangular Elements(TRIA3)				done
Stresses In Quadrilateral Elements(QUAD4)			done
Stresses In Quadrilateral Elements(QUAD4) option=bilin		done
Stresses In Layered Composite Elements(QUAD4)			done

Stresses In Tetrahedron Solid Elements(CTETRA)			done
Stresses In Hexahedron  Solid Elements(HEXA)			done
Stresses In Pentahedron Solid Elements(PENTA)			done

Strains In Bar Elements(CBAR)					done
Strains In Rod Elements(CROD)					done

Strains In Quadrilateral Elements(QUAD4)			done
Strains In Triangular Elements(TRIA3)				done

Strains In Tetrahedron Solid Elements(CTETRA)			done
Strains In Hexahedron  Solid Elements(HEXA)			done
Strains In Pentahedron Solid Elements(PENTA)			done


----LAMA - eigenvalues----
Real Eigenvalues						done
Complex Eigenvalue Summary					no object

----OUG----
Displacement Vector						done
Real Eigenvector No.						done
Complex Displacement Vector					done
Temperature Vector						done

***OEE - energy----
Element Strain Energies						???

----OGP - grid point force balance----
Grid Point Force Balance					???

***OPG - applied loads----
appliedLoadsObject						no
loadVectorObject						no

----not supported - main----
Nastran File And System Parameter Echo
Nastran Executive Control Echo
Case Control Echo
Model Summary

Element Geometry Test Results Summary
Output From Grid Point Weight Generator
OLoad Resultant
Maximum SPC Forces
Maximum Displacements
Maximum Applied Loads
Grid Point Singularity Table

----aero - not supported----
Non-Dimensional Stability And Control Derivative Coefficients
Non-Dimensional HingeMoment Derivative Coefficients
Aerostatic Data Recovery Output Tables
Structural Monitor Point Integrated Loads

----rotor - not supported----
Rotor Dynamics Summary
Rotor Dynamics Mass Summary
Eigen Value Analysis Summary(Complex Lanczos Method)
#------------------------




#----------------------------------------------------------------------------

F06 Reader
   - LAMA/CLAMA (requires an ESE = ALL to create op2 table)
     - eigenvalues  (real/***complex - no object)

   - OUG (DISPLACMENTS=ALL)
     - displacement (static/transient)
       - real/complex
     - velocity/acceleration (static/transient)
       - ***real/***complex
     - temperature  (static/transient)
     - eigenvectors (real/complex)

   - OQG (constraint forces; SPCFORCES=ALL, MPCFORCES=ALL)
     - SPC Forces (static/***transient)
     - MPC Forces (static/***transient)

   - OES (STRESS=ALL, STRAIN=ALL)
     - solid stress/strain (static/***transient)
        - CTETRA
        - CPENTA
        - CHEXA
     - isotropic plate stress/strain (static/***transient);  (directional vectors & pressure will be calculated, not stored)
        - CTRIA3
        - CQUAD4 (centroid/bilinear)
        - ***CQUAD8
        - ***CTRIA6
     - composite plate stress/strain (static/***transient)
        - CTRIA3
        - CQUAD4 (centroid)
        - ***CQUAD8
        - ***CTRIA6
     - rod stress/strain   (static/transient; CROD, CONROD, CTUBE)
     - bar stress/strain   (static/transient; CBAR)
     - ***beam  stress/strain (static/transient; CBEAM)
     - ***shear stress/strain (static/transient; CSHEAR)

#----------------------------------------------------------------------------

F06 Writer
   - OUG (DISPLACMENTS=ALL)
     - displacement (static/transient)
       - real/complex
     - velocity     (static/transient)
       - real
     - acceleration (static/transient)
       - real
     - temperature  (static/transient)
     - eigenvectors (real/***complex)

   - OES (STRESS=ALL, STRAIN=ALL)
     - solid stress/strain (static/transient);  (directional vectors & pressure calculated)
        - CTETRA
        - CPENTA
        - CHEXA
     - isotropic plate stress/strain (static/transient)
        - CTRIA3
        - CQUAD4 (centroid/bilinear)
        - ***CQUAD8
        - ***CTRIA6
     - composite plate stress/strain (static/transient)
        - CTRIA3
        - CQUAD4 (centroid)
        - ***CQUAD8
        - ***CTRIA6
     - rod stress/strain   (static/transient; CROD, CONROD, CTUBE)
     - bar stress/strain   (static/transient; CBAR)
     - beam  stress/strain (static/transient; CBEAM)
     - ***shear stress/strain (static/transient; CSHEAR)

   - LAMA/CLAMA (requires an ESE = ALL to create op2 table)
     - eigenvalues  (real/***complex)

   - OQG (constraint forces; SPCFORCES=ALL, MPCFORCES=ALL)
     - SPC forces (static/transient)
       - real/complex
     - MPC forces (static/transient)
       - real/complex

   - OGF (grid point forces; GPFORCES=ALL)
     - grid point force balance (static/transient)
     - load vector (static/transient)
