TY - GEN
T1 - Micro-scale thermal response modeling of an Avcoat-like TPS
AU - Sawant, Saurabh S.
AU - Rao, Pooja
AU - Harpale, Abhilash
AU - Chew, Huck Beng
AU - Levin, Deborah A.
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - The present work describes the efforts to model a complex microstructure of an Avcoat-like material using direct simulation Monte Carlo (DSMC) method with correct boundary conditions, where a cross flow of boundary layer and pyrolysis species through the material can be simulated. To aid in choosing the gas pressures at the boundary, the development and verification of a continuum scale, finite volume solver is presented that models the gas phase in conjunction with the solid phase. To understand the thermal response of the microstructure, a hybrid random walk model is described, which has a capability to include convection, conduction, and radiation. With the help of these tools, the relative importance of heat transfer mechanisms is analyzed on a micron scale morphology. Using DSMC, the continuum permeability of 15.7×10−12 m2 is obtained for our microstructure model with 0.71 porosity. Furthermore, the flow through the microstructure during the process of pyrolysis is analyzed and the detailed collision statistics are reported as a function of depth. An estimate of collision statistics along an assumed trajectory is given to show the relative importance of gas-gas and gas-surface collisions. In addition, a way to scale the DSMC results on a small scale sample to larger depths is described. Finally, molecular dynamics (MD) simulations based on reactive-force-field (ReaxFF) potential are performed to elucidate the pyrolysis kinetics of a highly crosslinked phenolic formaldehyde resin.
AB - The present work describes the efforts to model a complex microstructure of an Avcoat-like material using direct simulation Monte Carlo (DSMC) method with correct boundary conditions, where a cross flow of boundary layer and pyrolysis species through the material can be simulated. To aid in choosing the gas pressures at the boundary, the development and verification of a continuum scale, finite volume solver is presented that models the gas phase in conjunction with the solid phase. To understand the thermal response of the microstructure, a hybrid random walk model is described, which has a capability to include convection, conduction, and radiation. With the help of these tools, the relative importance of heat transfer mechanisms is analyzed on a micron scale morphology. Using DSMC, the continuum permeability of 15.7×10−12 m2 is obtained for our microstructure model with 0.71 porosity. Furthermore, the flow through the microstructure during the process of pyrolysis is analyzed and the detailed collision statistics are reported as a function of depth. An estimate of collision statistics along an assumed trajectory is given to show the relative importance of gas-gas and gas-surface collisions. In addition, a way to scale the DSMC results on a small scale sample to larger depths is described. Finally, molecular dynamics (MD) simulations based on reactive-force-field (ReaxFF) potential are performed to elucidate the pyrolysis kinetics of a highly crosslinked phenolic formaldehyde resin.
UR - http://www.scopus.com/inward/record.url?scp=85141640613&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85141640613&partnerID=8YFLogxK
U2 - 10.2514/6.2018-0495
DO - 10.2514/6.2018-0495
M3 - Conference contribution
AN - SCOPUS:85141640613
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 -