NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- A1.05-1052
SUBTOPIC TITLE:
 Computational Tools and Methods
PROPOSAL TITLE:
 Fast, Parallel, High-Quality Voronoi Mesh Generator
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
CASCADE Technologies, Inc.
2445 Faber Place, Suite 100
Palo Alto , CA 94303-3346
(650) 521-0243

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Michael Emory
memory@cascadetechnologies.com
2445 Faber Place, Suite 100 Palo Alto, CA 94303 - 3346
(650) 521-0243

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Guillaume Bres
gbres@cascadetechnologies.com
2445 Faber Place, Suite 100 Palo Alto, CA 94303 - 3346
(650) 521-0243
Estimated Technology Readiness Level (TRL) :
Begin: 6
End: 7
Technical Abstract

In this work we propose to further develop and demonstrate a mesh generation approach based on clipped Voronoi diagrams. This approach to mesh generation has the potential to significantly improve performance and robustness, while retaining important elements of high quality meshes including boundary alignment, stretching, and element regularity. Clipped Voronoi diagrams also automatically de-feature the underlying geometry at the local resolution of the generating points, and can thus significantly impact the problem of CAD clean-up and defeaturing.

The mathematical properties of Voronoi diagrams enable highly scalable mesh generation, since the global mesh is uniquely defined yet each individual cell can be constructed with only local information. Importantly the Voronoi paradigm reduces the problem of mesh generation to the much simpler problem of specifying the locations (point cloud) where the solution will be sampled. The actual mesh (volumes, faces, topology, neighbor connectivity) is simply a unique mathematical consequence of this choice. This dramatically simplifies control over local mesh resolution - an important consideration for automation and high-fidelity simulations. Additionally, the discretization of the boundary surface is independent from the near-boundary mesh resolution, allowing arbitrary coarsening or refinement relative to the local surface length scales. The impact of leveraging these benefits in mesh generation will be a dramatic reduction in the time and human interaction required to generate quality meshes for high-fidelity applications.

Understanding solution sensitivity to the point cloud parameters is the technical objective of the current proposal. We will asses solution sensitivity with respect to three different aspects related to the spatial arrangement of the point cloud. The cases investigated are relevant building blocks for aerodynamic problems of interest, i.e., the NASA Juncture Flow experiments.

Potential NASA Applications

Stitch's high-quality Voronoi meshes would benefit any solver utilizing polyhedral elements. Phase II will produce tools, specifically tetrahedral meshing and quadratures on regular polyhedra, that could benefit NASA's FEM solver, FUN3D, as well as it's DG and spectral-element solver, eddy. Charles, Cascade's massively parallel, low-dissipation multi-physics LES solver, leverages the properties of Voronoi meshes for accurate multi-physics, multiscale LES simulations could serve NASA engineers.

Potential Non-NASA Applications

Consumers utilizing Charles (e.g., gas-turbine sector of General Electric, aerothermodyanmics research at Honda, and fuel-injection research at Bosch) would benefit from the mesh efficiencies gained through our Phase I. Through demonstrations of mesh/solution quality, speed, scalability and workflow ease, we aim to increase the pool of consumers by making the push from a research and analysis framework to a true design tool.


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