Choosing the Analysis Procedure: Solid or Shell

Numerical simulation uses discrete approximations of continuum mechanics. Good numerical methods seek to balance accuracy, robustness, and performance.

The solid analysis procedure uses the finite volume method for Flow, Pack, and Cool analyses. This is a discrete approximation that applies equally to the three spatial dimensions. Results are more accurate when you use a fine mesh. However, you might decide to use a coarser mesh to achieve a faster, though less accurate solution.

The shell analysis procedure uses further numerical approximations to model the cross-stream flow and the heat transfer without using a mesh that spans the cross-stream direction. The shell analysis procedure applies primarily to thin parts with essentially uniform thickness.

The shell analysis procedure uses two numerical approximations to model laminar flow:
  • Hele-Shaw flow for cavity domains
  • Hagen-Poiseuille flow for runner domains
These approximations assume that the flow is always parallel to the solid boundaries, which means that the shell analysis procedure cannot properly model cross-stream flow. The shell analysis procedure is further limited to injection processes that use a single polymer material.
Hele-Shaw Flow for Shell Analysis Hagen-Poiseuille Flow for Shell Analysis
Laminar flow between two parallel flat plates separated by a small gap Laminar flow in a long cylindrical tube

The solid procedure typically requires a minimum of five mesh elements to span a flow passage. To mesh a thin part, you typically need at least five to ten times more solid mesh elements than shell elements. Judicious use of the shell procedure saves computation time.

The shell procedure will be less accurate wherever the basic assumption—that the flow is always parallel to the solid boundaries—is not valid. This can happen, for example, when the flow impinges on the cavity wall opposite a valve gate, when jetting occurs, or when a cavity flow encounters a protuberance or step change in thickness.

However, such inaccuracies might be local in nature and would have only small effects on the overall flow results. In addition, even though the solid procedure might be able to capture some or all of these effects, it also requires a fine enough mesh resolution to do so. Without sufficient mesh refinement, the solid procedure might not be significantly more accurate than the shell.

Recommendation: For accurate Cool and Warp analyses, use the solid procedure.

Recommended Analysis Procedure Based on Part Geometry

Part Geometry Example Shell Procedure Solid Procedure Comments
Thin parts with few or no thickness variations Yes Yes The shell procedure is most efficient for this type of part.
Thin parts Yes Yes The shell procedure can handle small variations in thickness and some holes in the part.
Thick parts No Yes  
Parts with large thickness variations No Yes  
Perforated plates No Yes The shell mesh procedure is suitable only in cases where the perforations are fewer or spaced far apart.
Grids No Yes  
Rings or frames No Yes  

Supported Injection Processes for Solid and Shell Procedures

Injection Process Solid Analysis Procedure Shell Analysis Procedure
Single Material Yes Yes
Single Material with Insert Yes No
Co-injection Yes No
Bi-injection Yes No
Gas-assist Yes No
Water-assist Yes No