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Computational Tool for Coupled Simulation of Nonequilibrium Hypersonic Flows…

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
95314
Program Year/Program:
2010 / SBIR
Agency Tracking Number:
094560
Solicitation Year:
N/A
Solicitation Topic Code:
X9
Solicitation Number:
N/A
Small Business Information
CFD Research Corporation
215 Wynn Dr., 5th Floor Huntsville, AL 35805-
View profile »
Woman-Owned: Yes
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2010
Title: Computational Tool for Coupled Simulation of Nonequilibrium Hypersonic Flows with Ablation
Agency: NASA
Contract: NNX10CC53P
Award Amount: $99,999.00
 

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.

Principal Investigator:

Sarma L. Rani
Principal Investigator
2567264850
slr@cfdrc.com

Business Contact:

Silvia Harvey
Documentation Specialist
2567264858
sxh@cfdrc.com
Small Business Information at Submission:

CFD Research Corporation
215 Wynn Drive, 5th Floor Huntsville, AL 35805

EIN/Tax ID: 630944385
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No