Abstract
Simulating high-speed combustion is computationally costly, motivating the development of tabulated chemistry models. One such model is the Evolution-Variable Manifold (EVM) approach, which precomputes and tabulates a representative chemical source term for use in a simulation at runtime. A variant of the EVM approach is proposed and discussed here which replaces the majority of these tabulated states with two pre-trained Artificial Neural Networks (ANNs). These ANNs use identical inputs and outputs to the original EVM model, but have been trained using data from a Reynolds-Averaged Navier-Stokes (RANS) flowfield with full finite-rate chemistry. This extends the EVM framework to all thermodynamic states within this flowfield, rendering the representation more robust. A proof-of-concept is shown, where a RANS simulation of a hydrogen jet in supersonic crossflow is conducted to verify the model against its training data. A Large-Eddy Simulation (LES) is conducted on the same configuration and compared to an LES with full finite-rate chemistry.
Original language | English (US) |
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Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624107115 |
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 The MITRE Corporation. Published by the American Institute of Aeronautics and Astronautics, Inc.