SBIR/STTR Research Award

Unified Kinetic/Continuum Flow Solver with Adaptive Cartesian Mesh for Hypersonic Flows in the Earth Atmosphere

Award identifier 0d7c604b3abf07f5f642f7fb00b9d374d3095c7fe91f0e073d397cd23b792244Awarding agency Department of Defense · Air Force

Award amount

$749,921

Program and phase

STTR · Phase II

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
2010-03-16
Contract end date
2012-03-16
UEI
V3KCP1HNFM33
Solicitation number
2008.A
Topic code
AF08-T019

Research abstract

The design of future hypersonic vehicles requires detailed understanding of flow regimes ranging from rarefied to continuum. Hypervelocity flows are characterized by high temperatures, real gas effects, nonequilibrium chemistry, and ionization. The goal of this project is to develop unified kinetic/continuum solution methods with automatic domain decomposition for a wide range of Air Force applications. The Unified Flow Solver (UFS) with Adaptive Mesh and Algorithm Refinement, developed by CFDRC, will be enhanced by advanced capabilities of the NASCART-GT viscous flow solver from Georgia Tech. The octree based Cartesian mesh methods used in both codes will be improved to better resolve viscous boundary layers and heat transfer simulations near surfaces. Phase I work has demonstrated the feasibility of an immersed boundary method to greatly improve heat transfer simulations with Cartesian mesh. UFS coupling with the general-purpose chemistry solver CANTERA allowed solving stiff chemistries for hypersonic flows. Adaptive mesh in velocity space was introduced to increase efficiency of the Boltzmann solver. During Phase II, these advanced numerical techniques will be incorporated into a user-friendly code. The code will be validated for heat transfer simulations with Cartesian mesh and demonstrated for several benchmark cases including heat transfer predictions in hypersonic rarefied, transitional and continuum flows. BENEFIT: The code will be used as a design tool for development of future hypersonic vehicles. In addition to Air Force applications, the code will be useful for a multitude of NASA technology development programs under Project Constellation and the New Millennium Program. Missile defense applications include Theater and Ballistic Missile Defense vehicles performing exo-atmospheric missile intercept, such as the Ground Based Midcourse Defense, Aegis, and Multi-Kill Vehicle programs. Commercial applications include material processing, vacuum science, and nanotechnologies.

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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