Abstract
This work presents an uncertainty and sensitivity analysis of the Modified Marrone–Treanor (MMT) model to evaluate the impact of uncertainties in quasiclassical trajectory (QCT) collision data-derived parameters. Two zero-dimensional reactor simulation cases were analyzed for preliminary sensitivity analysis, followed by two-dimensional hypersonic cylinder flow CFD simulations. Surrogate models enabled variance-based sensitivity analysis using Sobol indices to identify which reaction parameters most significantly impact the CFD outputs. Two cases were analyzed: one representative of shock tunnel experimental conditions and one of flight conditions. Results reveal that under experimental conditions, only the pre-exponential factors influence the solution, with negligible sensitivity to MMT-specific parameters. In contrast, flight conditions show substantial influence from the MMT parameters, suggesting that current shock tunnel experiments may not adequately constrain the parameters most relevant to flight prediction.
| Original language | English (US) |
|---|---|
| Title of host publication | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624107658 |
| DOIs | |
| State | Published - 2026 |
| Event | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026 - Orlando, United States Duration: Jan 12 2026 → Jan 16 2026 |
Publication series
| Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026 |
|---|
Conference
| Conference | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026 |
|---|---|
| Country/Territory | United States |
| City | Orlando |
| Period | 1/12/26 → 1/16/26 |
Bibliographical note
Publisher Copyright:© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
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