Abstract
The ultra-high temperature environment leads to surface oxidation of the carbon fiber, which could create non-uniform voids and weaken the integrity of the structure. A thorough thermal-chemical-structural coupling is conducted for carbon fiber using the developed new modeling technique. The evolving topology of the residue carbon fiber is captured by the simulation without actual moving grid manipulation. Current results show that for single carbon fiber, surface oxidation can be harmful since pitting can occur at multiple locations on the surface and pitting can penetrate the entire fiber. The variability of surface roughness, or sites, is also investigated by using a Gaussian function. It is found that when the surface is coarser, it becomes easier for carbon to be oxidized. The full coupling study will also be conducted to show that as oxidation continues within the materials, it becomes more vulnerable for the carbon fibers to withstand their loading.
Original language | English |
---|---|
Title of host publication | AIAA SciTech Forum 2022 |
DOIs | |
State | Published - 2022 |
Event | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States Duration: Jan 3 2022 → Jan 7 2022 |
Publication series
Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
---|
Conference
Conference | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
---|---|
Country/Territory | United States |
City | San Diego |
Period | 1/3/22 → 1/7/22 |
Bibliographical note
Publisher Copyright:© 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
Funding
The authors would like to thank Kristen Price for providing spallation experimental results for comparison. Financial support for this work was provided by The National Aeronautics and Space Administration Space Technology Research, Development, Demonstration, and Infusion (NASA SpaceTech-REDDI) Award 80NSSC18K0261 and Air Force of Office of Scientific Research 2020 (AFOSR) FA9550-18-1-0261."
Funders | Funder number |
---|---|
National Aeronautics and Space Administration Space Technology Research | |
National Aeronautics and Space Administration | 80NSSC18K0261 |
Air Force Office of Scientific Research, United States Air Force | FA9550-18-1-0261 |
ASJC Scopus subject areas
- Aerospace Engineering