TY - GEN
T1 - Comparison of Flamelet and Transported Species-Based Modeling of Rotating Detonation Engines
AU - Li, Wenhai
AU - Oh, Hyejin
AU - Ladeinde, Foluso
N1 - Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2024
Y1 - 2024
N2 - Limited research has incorporated detailed kinetic mechanisms in Computational Fluid Dynamics (CFD) simulations of Rotating Detonation Engines (RDE). Among these studies, the quasi-laminar (QL) approach is predominantly employed to capture the influence of turbulence on the reaction rate, given its simplicity. However, the impact of sub-grid scale turbulent-chemistry interaction modeling on RDE simulations remains largely unexplored. In this investigation, both flamelet-based and transported species-based models are utilized to explore combustion in the RDE, employing the framework of large eddy simulation. The simulations are conducted based on a two-dimensional unwrapped geometric model of the RDE. The transported species-based approach successfully establishes the baseline solution, and the applicability of the classical premixed level-set flamelet approach for reacting flow in the RDE is scrutinized. Ultimately, a modified premixed flamelet model is proposed for RDE simulation.
AB - Limited research has incorporated detailed kinetic mechanisms in Computational Fluid Dynamics (CFD) simulations of Rotating Detonation Engines (RDE). Among these studies, the quasi-laminar (QL) approach is predominantly employed to capture the influence of turbulence on the reaction rate, given its simplicity. However, the impact of sub-grid scale turbulent-chemistry interaction modeling on RDE simulations remains largely unexplored. In this investigation, both flamelet-based and transported species-based models are utilized to explore combustion in the RDE, employing the framework of large eddy simulation. The simulations are conducted based on a two-dimensional unwrapped geometric model of the RDE. The transported species-based approach successfully establishes the baseline solution, and the applicability of the classical premixed level-set flamelet approach for reacting flow in the RDE is scrutinized. Ultimately, a modified premixed flamelet model is proposed for RDE simulation.
UR - https://www.scopus.com/pages/publications/85195512033
U2 - 10.2514/6.2024-2599
DO - 10.2514/6.2024-2599
M3 - Conference contribution
AN - SCOPUS:85195512033
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -