Abstract
Fibrous materials are extensively employed as thermal protection system in aerospace engineering. In this paper, the effective thermal and mechanical properties of a carbon fibrous material are predicted based on representative volume element of the micro-structure using a nonlocal lattice particle method. The RVE is obtained by scanning the fibrous sample and outputting the structure information as voxel-based binary files. Specifically, we calculate the effective thermal conductivity tensor by solving a heat conduction problem with prescribed temperature boundary condition. We obtain the effective mechanical properties by running several designed tests with applied strain state.
Original language | English |
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Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
DOIs | |
State | Published - 2024 |
Event | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duration: Jan 8 2024 → Jan 12 2024 |
Publication series
Name | AIAA SciTech Forum and Exposition, 2024 |
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Conference
Conference | AIAA SciTech Forum and Exposition, 2024 |
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Country/Territory | United States |
City | Orlando |
Period | 1/8/24 → 1/12/24 |
Bibliographical note
Publisher Copyright:© 2024 by Donglai Liu and Hailong Chen.
ASJC Scopus subject areas
- Aerospace Engineering