SBIR/STTR
An Automated High Aspect Ratio Mesher for Computational Fluid Dynamics, Phase II
Project Introduction
Computational fluid dynamics (CFD) simulations are routinely used while designing, analyzing, and optimizing air- and spacecraft. An important component of CFD simulations is mesh generation, or discretization into polygonal or polyhedral cells, of the domain being analyzed. The work will focus on the 3D implementation of the Phase 1 CHARM mesher, with solution-adaptive iteration for CFD and non-CFD applications. The proposed 3D method will incorporate and extend a previously developed method of generating field-guided hexahedral elements from a metric tensor field. While the fundamental technical approach -- a combination of metric tensor conditioning, metric-tracing mesher, and cell-packing mesher -- remains the same, there are many technical challenges specific to the 3D domain, including the following: - Investigation into conditioning of volume metric tensor fields - Investigation into the topology (structure) of volume metric tensor fields - Developing algorithms for the generation, repair, and adjustment of streamsurface arrangements - Developing algorithms to convert streamsurface arrangements to hex-dominant meshes - Developing algorithms to combine streamsurface- and packing-based meshes - Investigation into designing these algorithms for mesh adaptation rather than adaptive remeshing - Investigation of time and storage efficiency of these algorithms in a large-scale parallelism context In addition to the above, the goal is to generalize the solution in order to support its packaging and commercialization for a number of problem sets and target applications. This includes generalization of the solver-adaptive framework, creation of APIs to programatically expose core functions, and provide UI access to appropriately control and configure the application.
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Anticipated Benefits
The Ciespace adaptive remeshing framework can be applied to the evaluation, design/redesign, and assessment of air- and spacecraft for current and future NASA missions. The current requirement is the use of a suitable CFD solver which can take mixed-element meshes as input for solution and provide metric output for adaptive refinement. The following represent example applications in three categories: 1. Evaluation ? Evaluating the initial design space for future missions by complementing experimental studies with simulation results. This can be applied to the modeling of air (terrestrial and otherwise) and space vehicles under various conditions. 2. Design/Redesign ? Making design decisions or modifications to existing designs based on predictive simulation and experimental validation of concepts. 3. Assessment ? Determining the flight-dynamics of current platforms (Constellation vehicles, the Mars ARES scout, and others). This may lead to redesign activities. The proposed innovation can be leveraged by Ciespace to address commercial problems in a number of categories: ? CFD analysis problems with high-flow conditions and defined flow feature orientations. ? High-deformation problems in impact, crash, or thermal change. ? Analysis of high stress or vibration across a model. ? Electromagnetic analysis driven by varying field conditions across a surface or volume. These problem sets are applicable across a number of markets, including aerospace, automotive, electronics, and heavy equipment manufacturing, serving large-scale enterprises as well as mid-market parts suppliers. Inclusion of the innovation in the Ciespace integrated solution supports differentiation in the product through improved control over high aspect ratio meshes, as well as the ability to demonstrate tighter bi-directional integration with industry solver technologies addressing these problems, including: ? CFD solvers, such as Fluent, FUN3D, and others ? Injecti
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Marshall Space Flight Center
(MSFC)
|
Lead Organization | NASA Center | Huntsville, AL |
| Ciespace Corporation | Supporting Organization | Industry | Oak Brook, IL |
Primary U.S. Work Locations
-
Alabama
-
Illinois
-
Virginia
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Marshall Space Flight Center (MSFC)
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Project Manager:
Principal Investigator:
- Kenji Shimada
Project Duration
Start: Aug 2011
End: Feb 2014
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 3 |
| Estimated End: | 6 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX15 Flight Vehicle Systems
- TX15.1 Aerosciences
- TX15.1.3 Aeroelasticity
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