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Gas-Kinetic Simulation of Separated Flows

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W31P4Q-09-C-0090
Agency Tracking Number: 07SB2-0071
Amount: $749,891.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: SB072-006
Solicitation Number: 2007.2
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-12-15
Award End Date (Contract End Date): 2011-03-14
Small Business Information
3409 N. 42nd Pl.
Phoenix, AZ 85018
United States
DUNS: 781820258
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Lei Tang
 (480) 518-0981
Business Contact
 Lei Tang
Title: President
Phone: (480) 518-0981
Research Institution

This SBIR project proposes to develop a gas-kinetic CFD solver for separated turbulent flow simulation. After successfully developing prototype two-dimensional gas-kinetic BGK-NS/Burnett solvers and demonstrating the benefits of using higher-order hydrodynamic equations for separated turbulent flow simulation in Phase I, the technical objective of Phase II work will be to fully develop and validate the gas-kinetic BGK-Burnett solver for real aerospace applications. We will continue to improve the robustness, accuracy and computational efficiency of the gas-kinetic BGK-NS/Burnett solvers; to extend the solver to three-dimensional curvilinear coordinates; to develop a new set of nonlinear turbulence model for the gas-kinetic BGK-Burnett solver based on the so-called RNG (Renormalization Group) Analysis; to develop the implicit solvers for both BGK-Burnett solver and the turbulence model. The outcome of our Phase II work will be a validated gas-kinetic CFD software product ready for commercialization.

* Information listed above is at the time of submission. *

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