SBIR/STTR Research Award

SBIR Phase I: A Fast Parallel Grid-Free Method for Simulating Turbulent Incompressible Flow In/Around Time-Varying Geometries

Award identifier e95c6381b214ee72ba3153eb6c4182b3bf7367a6b77475b0a4c05b2543626739Awarding agency National Science Foundation

Award amount

$84,338

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
National Science Foundation
Branch
Not reported
Recipient company
Applied Scientific Research
Proposal award date
Not reported
Contract end date
Not reported
UEI
TWVCT2J45887
Solicitation number
Not reported
Topic code
Not reported

Research abstract

This Small Business Innovation Research (SBIR) Phase I project prepares the ground-work for the development of the first commercially available Computational Fluid Dynamics package for a truly grid-free Large Eddy Simulation (LES) of turbulent incompressible vortex dominated flow in complex time-varying geometries. The computational engine is based on the parallel, fast multi-pole implementation of a Lagrangian vortex-boundary element method. Turbulence is accounted for via LES, using a Lagrangian dynamic Smagorinsky sub-grid scale model. The method is: (1) fully grid-free in the fluid domain, (2) free of numerical diffusion, (3) inherently solution-adaptive, and (4) capable of modeling inhomogeneous unsteady wall-bounded turbulent flow. To this end, two new ideas will be developed during Phase I: A grid-free method for predicting diffusion with variable-viscosity, which is a pre-requisite for LES modeling; and a non-diffusive vortex merging strategy to curb the proliferation of particles and maintain long-time accuracy. These will then be incorporated into the Lagrangian vortex element method to demonstrate the salient features of grid-free vortex-based LES modeling of turbulent flows, using the prototypical example of the evolution of an initially perturbed infinite-Reynolds-number vortex ring in free space. The software is ideal for simulation and analysis of complex turbulent flow phenomena. This includes vortex breakdown, (massive) flow separation, vortex shedding, transient jets in cross-stream, wake-body interaction, high-swirl flow, etc. All are associated with the design of advanced flow control mechanisms used, for example, to reduce flow-induced noise and vibration, and to improve lift/drag performance at reduced energy consumption rates. Examples are flow over bluff bodies such as ground or under-water vehicles; in engines; in/around rotating machinery such as pumps and fans; helicopters; or in data storage units with rotating and moving parts.

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

9 SBIR/STTR records share this UEI (2001–2012). Reported award amounts total $2,308,091. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Science Foundation

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