TY - GEN
T1 - Prediction of thermal protection system material permeability and hydraulic tortuosity factor using Direct Simulation Monte Carlo
AU - Jambunathan, Revathi
AU - Levin, Deborah A.
AU - Borner, Arnaud
AU - Ferguson, Joseph C.
AU - Panerai, Francesco
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Carbon 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 of two types of carbon preforms, namely, Morgan Felt and FiberForm, and assessed the effect of orientation of the permeability. It was found that for both the anisotropic materials, the permeability is higher in the in-plane orientation compared to the through-thickness orientation. Compared to Morgan Felt, FiberForm is less permeable, in both, through thickness and in-plane directions. The hydraulic tortuosity was higher for the FiberForm compared to Morgan Felt, and it was also found that the through-thickness orientation is more tortuous compared to the in-plane orientation.
AB - Carbon 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 of two types of carbon preforms, namely, Morgan Felt and FiberForm, and assessed the effect of orientation of the permeability. It was found that for both the anisotropic materials, the permeability is higher in the in-plane orientation compared to the through-thickness orientation. Compared to Morgan Felt, FiberForm is less permeable, in both, through thickness and in-plane directions. The hydraulic tortuosity was higher for the FiberForm compared to Morgan Felt, and it was also found that the through-thickness orientation is more tortuous compared to the in-plane orientation.
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U2 - 10.2514/6.2018-0497
DO - 10.2514/6.2018-0497
M3 - Conference contribution
AN - SCOPUS:85141589976
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -