TY - GEN
T1 - High fidelity and multi-scale thermal response modeling of an Avcoat-like thermal protection system material
AU - Sawant, Saurabh S.
AU - Harpale, Abhilash
AU - Jambunathan, Revathi
AU - Chew, Huck Beng
AU - Levin, Deborah A.
N1 - Funding Information:
The research is being performed at the University of Illinois Urbana-Champaign is supported by an Early Stage Innovation (ESI) NASA Grant No. NNX 16AD12G with computer time on NASA/Pleiades - Award STMD-16-676 and the Blue Waters sustaincd-petascale computing project, which is supported by the National Science Foundation (awards OCI-0725070 and ACI-1238993) and the state of Illinois. Blue Waters is a joint effort of the University of Illinois at Urbana-Champaign and its National Center for Supercomputing Applications
Publisher Copyright:
© 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2017
Y1 - 2017
N2 - This paper presents a high fidelity, multi-scale thermal response models for a multiphase syntactic foam as a candidate Thermal Protection System (TPS) material, similar to AVCOAT. Scale-bridging molecular dynamics (MD) simulations are used to characterize the ablation chemistry and to obtain the thermal recession rate. The latter is used in Direct Simulation Monte Carlo (DSMC) simulations to model gas transport, heat transfer, and TPS material recession at the meso-scale level utilizing a strategy to loosely couple DSMC with the thermal response of the syntactic foam. The effect of interstitial void fraction on the steady state temperature profile of the material structure is explored.
AB - This paper presents a high fidelity, multi-scale thermal response models for a multiphase syntactic foam as a candidate Thermal Protection System (TPS) material, similar to AVCOAT. Scale-bridging molecular dynamics (MD) simulations are used to characterize the ablation chemistry and to obtain the thermal recession rate. The latter is used in Direct Simulation Monte Carlo (DSMC) simulations to model gas transport, heat transfer, and TPS material recession at the meso-scale level utilizing a strategy to loosely couple DSMC with the thermal response of the syntactic foam. The effect of interstitial void fraction on the steady state temperature profile of the material structure is explored.
UR - http://www.scopus.com/inward/record.url?scp=85017223033&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85017223033&partnerID=8YFLogxK
U2 - 10.2514/6.2017-0438
DO - 10.2514/6.2017-0438
M3 - Conference contribution
AN - SCOPUS:85017223033
T3 - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
BT - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 55th AIAA Aerospace Sciences Meeting
Y2 - 9 January 2017 through 13 January 2017
ER -