SBIR/STTR Research Award

High-Fidelity Simulation of Hypersonic Weakly Ionized Plasmas with Dynamically Adaptive Mesh

Award identifier 86ff75aeff3802c84d2e0392c9ac7e8ddcc2a08545ff0e5fcb173bb34d51e930Awarding agency Department of Defense · Air Force

Award amount

$99,994

Program and phase

STTR · Phase I

Award year

2010

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
CFD Research Corporation
Proposal award date
2010-05-01
Contract end date
2011-01-31
UEI
V3KCP1HNFM33
Solicitation number
2009.B
Topic code
AF09-BT10

Research abstract

The goal of the proposed research is to develop advanced computational tool for high-fidelity simulations of hypersonic non-equilibrium plasmas. Octree adaptive Cartesian mesh will be used for automatic mesh generation and dynamic mesh adaptation to plasma properties, particularly important for hypersonic flows with strong shock waves, transient laminar and turbulent domains with large gradients of flow parameters, and complex geometries. The plasma model will be applicable for both high temperature and low-temperature non-equilibrium weakly ionized flows and include a Boltzmann solver for electrons. This project will combine previous experience of the University of Michigan group in hypersonic plasmas with CFDRC experience in electron kinetics and gas discharge plasmas. The Unified Flow Solver developed at CFDRC for simulations of rarefied and continuum flows will be used as a framework. During Phase I, we will assemble the developed physical models and numerical algorithms into a prototype computational tool for adaptive multi-scale plasma simulations. In Phase II, the proposed software will be fully developed and validated for several benchmark cases of interest to the Air Force. We will demonstrate the new capabilities for hypersonic external flows and study communication blackout and plasma flow control by electromagnetic fields. BENEFIT: The developed computational tool will be utilized for evaluation of plasma phenomena on hypersonic vehicles and ground test facilities. The target applications will include hypersonic flight problems, electric propulsion, and plasma plumes expanding through nozzles. The methodology and software will be extendable for analysis of high-speed plasma jets for material processing and biomedical applications, plasma assisted ignition and combustion. Potential users include Air Force, NASA, and commercial companies utilizing plasma technologies for aerospace, propulsion, power, material processing, and other applications.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

947 SBIR/STTR records share this UEI (1987–2026). Reported award amounts total $350,893,199. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, National Science Foundation, Department of Commerce, Department of Energy

Agency intelligence

Department of Defense

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