We study modular code generation from SBDs: modular means that code is generated for a given composite block independently from context (i.e., without knowing in which diagrams this block is to be used).
Omni strain failure envelopes are proposed as the minimum inner failure envelope in strain space, which defines the failure of a given composite material for all ply orientations.
A direct method is also developed to determine the steady-state characteristics from just the initial conditions and configurations of a given composite system.
Property closures delineate the complete set of feasible effective property combinations in a given composite material, and are of tremendous interest in highly constrained design applications.
The effective coefficients are universal in nature and once determined, can be used to examine a number of boundary value problems associated with a given composite geometry.
The 3D stress behavior at the free edge of the composite patch is modeled by Lekhnitskii stress functions, and the governing equations of the given composite patch are obtained by applying the principle of complementary virtual work.
The temperature dependence of the anisomorphic CFL diagram for a given composite is characterized by the temperature dependence of the static strengths in tension and compression and of the reference S N relationship for a critical stress ratio.
Or to take a more concrete example, the existence of any given composite object is grounded in the existence of its parts.
For example, there are properties of composite (i.e. non-prime) numbers which can be shown to hold in relation to about half of the numbers less than a given composite number.
