Abstract
Carbon surfaces exposed to hypersonic flow are susceptible to oxidation and nitridation by the surrounding partially dissociated air. The Air-Carbon Ablation (ACA) model is a recently developed finite-rate oxidation and nitridation model anchored with data from molecular beam experiments. Although the ACA model contains rates for the dominant oxidation and nitridation processes, it does not contain backward rates. In this work, the ACA model is extended. Backward rates are derived for the model to allow CO, CO2, and CN to interact with the surface. Temperature-dependent scaling factors are formulated to ensure the model reaches a thermochemical equilibrium state consistent with mimimizing the Gibbs energy of the carbon-air system.
Original language | English |
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Title of host publication | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 |
DOIs | |
State | Published - 2025 |
Event | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 - Orlando, United States Duration: Jan 6 2025 → Jan 10 2025 |
Publication series
Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 |
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Conference
Conference | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 |
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Country/Territory | United States |
City | Orlando |
Period | 1/6/25 → 1/10/25 |
Bibliographical note
Publisher Copyright:© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
ASJC Scopus subject areas
- Aerospace Engineering