SBIR/STTR Research Award

Fast, Parallel, High-Quality Voronoi Mesh Generator

Award identifier 216fdf7956015065d18a4463fbeaaa0e155826feb663bf8e3a9b4b4f3dbbb2e5Awarding agency National Aeronautics and Space Administration

Award amount

$124,704

Program and phase

SBIR · Phase I

Award year

2018

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
CASCADE TECHNOLOGIES INC
Proposal award date
2018-07-27
Contract end date
2019-02-15
UEI
K9KCLNBFQAF6
Solicitation number
SBIR_18_P1
Topic code
A1

Research 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 diagramsenable 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 thelocations (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 surfaceis 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.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

47 SBIR/STTR records share this UEI (2004–2022). Reported award amounts total $21,363,179. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

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