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Prediction of Thermal Protection System Material Permeability and Hydraulic Tortuosity Factor Using Direct Simulation Monte CarloCarbon preforms used in Thermal Protection System (TPS) materials are 80 to 90% porous, allowing for boundary layer and pyrolysis gases to flow through the porous regions. The bulk material properties such as permeability and hydraulic tortuosity factor affect the transport of the boundary layer gases. The use of Direct Simulation Monte Carlo along with the Klinkenberg permeability formulation allows us to compute the continuum permeability and Knudsen correction factor for flow in the transition regime. In this work, we have computed the permeability for two types of carbon preforms, namely, Morgan Felt and FiberForm, and assessed the effect of orientation on the permeability. Since both the materials are anisotropic, the permeability was found to depend on orientation, wherein, the materials are more permeable in the in-plane orientation than the through-thickness orientation. The through-thickness orientation was also more tortuous compared to the in-plane material orientation. Compared to Morgan Felt, FiberForm is less permeable, in both, through thickness and in-plane directions.
Document ID
20190026637
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Jambunathan, Revathi
(Illinois Univ. Urbana-Champaign, IL, United States)
Levin, Deborah A.
(Illinois Univ. Urbana-Champaign, IL, United States)
Borner, Arnaud
(Science and Technology Corp. Moffett Field, CA, United States)
Ferguson, Joseph C.
(NASA Ames Research Center Moffett Field, CA, United States)
Panerai, Francesco
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
June 25, 2019
Publication Date
January 8, 2018
Subject Category
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN50011
Meeting Information
Meeting: AIAA SciTech 2018
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
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