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A three dimensional Computer Aided Design (CAD) model of a composite part to include a plurality of plies is described. The model includes an explicit representation for each individual ply utilized to form the composite part, where each individual ply is created as one of a solid or tessellated vol

A three dimensional Computer Aided Design (CAD) model of a composite part to include a plurality of plies is described. The model includes an explicit representation for each individual ply utilized to form the composite part, where each individual ply is created as one of a solid or tessellated volume. Each ply representation is in a proper spatial orientation with related component definitions.

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What is claimed is: 1. A computer readable medium with computer instructions embedded thereon, which, when executed, generate a three dimensional Computer Aided Design (CAD) model of a composite part to include a plurality of plies, the model including an explicit representation for each individual

What is claimed is: 1. A computer readable medium with computer instructions embedded thereon, which, when executed, generate a three dimensional Computer Aided Design (CAD) model of a composite part to include a plurality of plies, the model including an explicit representation for each individual ply utilized to form the composite part, each individual ply created as one of a solid format or a closed tessellated volume format, each said representation located in proper spatial orientation with related component definitions. 2. The computer readable medium according to claim 1 wherein said explicit representation of the individual plies includes instructions configured to create an inseparable assembly construct. 3. The computer readable medium according to claim 1 wherein for a closed tessellated volume format representation of an individual ply, each tessellation or facet is a planar approximation of a ply's surface having a fidelity sufficient to retain a design intent. 4. The computer readable medium according to claim 1 wherein said explicit representation of the individual plies comprises an attribute that indicates an orientation of an individual ply with respect to theoretical directions represented in the composite design. 5. The computer readable medium according to claim 1 wherein said explicit representation of the individual plies includes data in a closed faceted volume of sufficient fidelity to convey design intent. 6. The computer readable medium according to claim 1 wherein said model further comprises at least one of inserts, cores, and subsystems included with said plies. 7. The computer readable medium according to claim 1 wherein said model is presented in a defined format that can be converted into a format that provides a closed tessellated volumetric representation. 8. A method for explicitly representing individual plies of a composite structure, said method comprising: defining the individual plies of the structure; creating the individual ply definitions in a tessellated volume representation for each ply; utilizing the tessellated volume representations for the individual plies to generate a three dimensional design intent representation for the composite structure; describing the tessellated volumes in a format compatible with re-purposing to one or more computer-based viewer programs. 9. A method according to claim 8 wherein the tessellated volume representation comprises a position of each triangle of the tessellated volume with respect to a reference and a definition of how the triangles are interconnected. 10. A method according to claim 8 wherein describing the tessellated volumes in a format comprises converting the tessellated volumes into a defined format that provides a closed tessellated volumetric representation. 11. A method according to claim 8 wherein defining the individual plies of the structure comprises displaying every ply in the structure as a solid. 12. A method according to claim 8 wherein defining the individual plies of the structure comprises displaying the plies in a quasi-realistic stacking sequence with respect to one another. 13. A method according to claim 8 further comprising representing any holes or other discontinuities associated with ply definition. 14. A method according to claim 8 wherein describing the tessellated volumes in a format comprises at least one of providing an ability to see where the stacks of plies are, providing an ability to display how the plies relate to one another, providing an ability to cross-section the resulting component at any place, at any time, without the use of a specific composite tool. 15. A method according to claim 8 wherein defining the individual plies of the structure comprises including an attribute that indicates a location of the ply with respect to at least one other ply, defining a geometry of the ply, a material used to make the ply and indicating a materials orientation with respect to a theoretical coordinate system. 16. A method according to claim 8 wherein defining the individual plies of the structure comprises conveying design intent for the structure. 17. A method according to claim 8 wherein utilizing the tessellated volume representations of the individual plies to generate a three dimensional design intent representation comprises stacking the tessellated volume representations of the individual plies to generate an overall representation of the laminate composite structure. 18. A method according to claim 8 wherein utilizing the tessellated volume representations of the individual plies to generate a three dimensional design intent representation for the structure further comprises providing a capability to determine a thickness of the composite structure at any particular point of the structure. 19. A method according to claim 8 wherein utilizing the tessellated volume representations of the individual plies to generate a three dimensional design intent representation for the structure further comprises providing a capability to calculate a volume for an individual ply utilizing material properties associated with the particular ply. 20. A method according to claim 19 further comprising calculating a weight for, the composite structure utilizing the material properties and volumes associated with the individual plies. 21. A system comprising: a first computer configured with a computer aided design program operable to generate one or more computer files that explicitly represent individual plies of a composite structure in a format compatible with re-purposing to one or more computer-based viewer programs; and a storage device configured for storage of the one or more computer files. 22. A system according to claim 21 wherein said storage device is communicatively coupled to said first computer via a computer network, said system further comprising a second computer communicatively coupled to said storage device via the computer network, said second computer configured with a viewer program operable for viewing the representations of the individual plies by accessing the one or more computer files. 23. A system according to claim 21 wherein to explicitly represent individual plies of a composite structure, said first computer is programmed to create each individual ply definition as one of a solid format or a closed tessellated volume format, each individual ply definition located in proper spatial orientation with related component definitions. 24. A system according to claim 21 wherein to explicitly represent individual plies of a composite structure, said first computer is programmed to: create the individual ply definitions in a tessellated volume representation for each ply; and utilizing the tessellated volume representations for the individual plies to generate a three dimensional design intent representation for the composite structure, the tessellated volume representations in a format compatible with the viewer program.