Computational Tool for Coupled Simulation of Nonequilibrium Hypersonic Flows with Ablation

Award Information
Agency:
National Aeronautics and Space Administration
Branch:
N/A
Amount:
$99,999.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
NNX10CC53P
Agency Tracking Number:
094560
Solicitation Year:
2009
Solicitation Topic Code:
X9.01
Solicitation Number:
N/A
Small Business Information
CFD Research Corporation
215 Wynn Drive, 5th Floor, Huntsville, AL, 35805-1944
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
Y
Duns:
185169620
Principal Investigator
 Sarma Rani
 Principal Investigator
 (256) 726-4850
 slr@cfdrc.com
Business Contact
 Silvia Harvey
Title: Documentation Specialist
Phone: (256) 726-4858
Email: sxh@cfdrc.com
Research Institution
N/A
Abstract
The goal of this SBIR project is to develop a computational tool with unique predictive capabilities for the aerothermodynamic environment around ablation-cooled hypersonic re-entry vehicles. The framework for this tool will be developed such that all relevant models can be coupled to the LeMANS code for nonequilibrium hypersonic flows and the MOPAR code for ablation material response, both developed by the University of Michigan. In the proposed effort, the existing LeMANS-MOPAR framework will be enhanced by including innovative models for: (1) Non-equilibrium surface thermochemistry; (2) Non-equilibrium pyrolysis chemistry; (3) Radiation transfer in media with orders of magnitude variation in optical thickness; and (4) Spallation. The proposed tool is comprehensive and unique because all important phenomena will be modeled, with the software framework enabling coupling between the various components. The Phase I focus will be to: (1) Develop a module for the Modified Differential Approximation (MDA) to solve the radiative transfer equation; (2) Develop a framework for coupling the MDA module to LeMANS-MOPAR; and (3) Demonstrate the coupled framework for cases such as the Stardust re-entry. In Phase II, the tool will be made comprehensive by implementing important models identified above, including advanced non-equilibrium, non-gray radiation model. The tool will be validated and applied to re-entry ablation flows relevant to NASA. We will team with an ablative material OEM and a CFD software vendor to transition the technology to industry.

* information listed above is at the time of submission.

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