Masters Theses
Keywords and Phrases
Ablation; CFD; Fluent; Hypersonics; Material Response; Surface Chemistry
Abstract
Accurate prediction of ablative thermal protection system (TPS) performance is critical for hypersonic vehicle design. However, numerical prediction of ablation remains challenging because results are influenced by complex physics and the choice of surface chemistry model and assumptions made in material response calculations. The objective of this work is to evaluate several carbon ablation models and their implementation within modern computational fluid dynamics (CFD) codes. Numerical simulations were performed using NASA’s LAURA flow solver and the commercial CFD code ANSYS Fluent, which coupled Navier-Stokes with surface chemistry models describing carbon oxidation, nitridation, and sublimation reactions. Several reaction sets were considered, including the Park, LAURA, Duffa, and Zhluktov & Abe (ZA) models. Simulations were conducted in arc-jet and free flight conditions with comparisons performed between codes for non-ablating, steady-state ablation, and transient material response simulations. Validation and comparison studies demonstrated generally good agreement between codes and with experiments, with differences in wall temperatures and heat fluxes being generally less than 2%. Comparisons between surface chemistry models in Fluent showed that the Park and LAURA models produce similar ablation rates in oxidation-dominated conditions, whereas the Duffa and ZA models predict substantially lower ablation rates. However, the models predicted increasingly similar ablation rates as the sublimation reactions become dominant. Comparisons between steady-state and material response simulations further demonstrate that neglecting transient conduction within the solid can affect predicted surface temperatures and recession behavior.
Advisor(s)
Hosder, Serhat
Committee Member(s)
Crawford, Bruce
Vigano, Davide
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Aerospace Engineering
Publisher
Missouri University of Science and Technology
Publication Date
Spring 2026
Pagination
xiv, 162 pages
Note about bibliography
Includes_bibliographical_references_(pages 149-158)
Rights
© 2026 Andrew Steven Heider , All Rights Reserved
Document Type
Thesis - Open Access
File Type
text
Language
English
Thesis Number
T 12595
Recommended Citation
Heider, Andrew Steven, "Assessment and Comparison of Selected Carbon Ablation Models in Hypersonic Free-Flight and Arc-Jet Conditions" (2026). Masters Theses. 8279.
https://scholarsmine.mst.edu/masters_theses/8279
