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Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Helden Aerospace Corporation
- Proposal award date
- 2022-07-21
- Contract end date
- 2023-01-25
- UEI
- KZC3LFDHAN38
- Solicitation number
- SBIR_22_P1
- Topic code
- A1
Research abstract
Successful completion of our Phase I effort results in development and delivery of an enhanced version of HeldenMesh demonstrated for accurate, efficient, and automated CFD mesh generation for WMLES applications.nbsp;nbsp;HeldenMesh is an existing commercial CFD mesh generator already in widespread use in industry and NASA for generating meshes for Navier-Stokes CFD flow solvers like FUN3D and USM3D.nbsp;nbsp;It was originally developed under Helden internal research and recently enhanced under several NASA and Air Force Research Laboratory (AFRL) funded SBIR efforts.nbsp;nbsp;Our proposed effort builds upon these past efforts by incorporating two enhancements to enable more accurate and robust WMLES simulations.nbsp;nbsp;First, HeldenMesh is modified to generate a quad-dominated surface mesh and a hex-dominated near-wall layer mesh for a more efficient and accurate cell type which is more suited to WMLES analysis.nbsp;nbsp;Second, HeldenMesh is modified to generate wedge elements in the viscous layers at sharp trailing edges to improve the overall grid quality and grid normal alignment.nbsp;nbsp;Any further development required to improve HeldenMeshrsquo;s WMLES mesh generation capability is identified under Phase I and plans made for completion under a follow-on Phase II.nbsp;nbsp;With these enhancements in place, we then demonstrate the accuracy and efficiency of HeldenMesh for WMLES applications using the FUN3D flow solver on two test cases coordinated with NASA.nbsp;nbsp;As part of these demonstrations, WMLES meshing best practices are developed in terms of grid quality, impact of anisotropic stretching near and far from the wall vs. isotropic meshing, number of viscous layers, layer growth rate/profiles, as well as spanwise/chordwise spacing requirements in the critical near-wall regions.nbsp;nbsp;A grid convergence study is also performed with impact of cell count in critical regions vs. accuracy.nbsp;nbsp;Our effort culminates with delivery of an enhanced HeldenMesh executable with a direct FUN3D interface for independent testing.
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
6 SBIR/STTR records share this UEI (2017–2023). Reported award amounts total $2,740,583. Reported amounts are not federal obligations.
Phases: Phase II, Phase I
Agencies: National Aeronautics and Space Administration
Agency intelligence
National Aeronautics and Space Administration
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