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Validation of a Three-Dimensional Ablation and Thermal Response Simulation CodeThe 3dFIAT code simulates pyrolysis, ablation, and shape change of thermal protection materials and systems in three dimensions. The governing equations, which include energy conservation, a three-component decomposition model, and a surface energy balance, are solved with a moving grid system to simulate the shape change due to surface recession. This work is the first part of a code validation study for new capabilities that were added to 3dFIAT. These expanded capabilities include a multi-block moving grid system and an orthotropic thermal conductivity model. This paper focuses on conditions with minimal shape change in which the fluid/solid coupling is not necessary. Two groups of test cases of 3dFIAT analyses of Phenolic Impregnated Carbon Ablator in an arc-jet are presented. In the first group, axisymmetric iso-q shaped models are studied to check the accuracy of three-dimensional multi-block grid system. In the second group, similar models with various through-the-thickness conductivity directions are examined. In this group, the material thermal response is three-dimensional, because of the carbon fiber orientation. Predictions from 3dFIAT are presented and compared with arcjet test data. The 3dFIAT predictions agree very well with thermocouple data for both groups of test cases.
Document ID
20100035735
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Chen, Yih-Kanq
(NASA Ames Research Center Moffett Field, CA, United States)
Milos, Frank S.
(NASA Ames Research Center Moffett Field, CA, United States)
Gokcen, Tahir
(Eloret Corp. Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
June 28, 2010
Subject Category
Mathematical And Computer Sciences (General)
Report/Patent Number
ARC-E-DAA-TN1722
Report Number: ARC-E-DAA-TN1722
Meeting Information
Meeting: 10th AIAA/ASME Joint Thermophysics and Heat Transfer
Location: Chicago, IL
Country: United States
Start Date: June 28, 2010
End Date: July 1, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 599489.02.07.01.04
CONTRACT_GRANT: NNA04BC25C
Distribution Limits
Public
Copyright
Public Use Permitted.
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