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Development of a Three-Dimensional, Unstructured Material Response Design ToolA preliminary verification and validation of a new material response model is presented. This model, Icarus, is intended to serve as a design tool for the thermal protection systems of re-entry vehicles. Currently, the capability of the model is limited to simulating the pyrolysis of a material as a result of the radiative and convective surface heating imposed on the material from the surrounding high enthalpy gas. Since the major focus behind the development of Icarus has been model extensibility, the hope is that additional physics can be quickly added. This extensibility is critical since thermal protection systems are becoming increasing complex, e.g. woven carbon polymers. Additionally, as a three-dimensional, unstructured, finite-volume model, Icarus is capable of modeling complex geometries. In this paper, the mathematical and numerical formulation is presented followed by a discussion of the software architecture and some preliminary verification and validation studies.
Document ID
20180002975
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Schulz, Joseph C.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Stern, Eric C.
(NASA Ames Research Center Moffett Field, CA, United States)
Muppidi, Suman
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Palmer, Grant E.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Schroeder, Olivia
(Kentucky Univ. Louisville, KY, United States)
Date Acquired
May 21, 2018
Publication Date
January 9, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Mathematical And Computer Sciences (General)
Report/Patent Number
ARC-E-DAA-TN38048
Report Number: ARC-E-DAA-TN38048
Meeting Information
Meeting: AIAA SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
CONTRACT_GRANT: NNX15AD73G
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Thermal Protection System
Ablation
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