LES Model Assessment for High Speed Combustion
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. LES Model Assessment for High Speed Combustion using Mesh-Sequenced Realizations
2. Large-eddy/Reynolds-averaged Navier–Stokes simulation of a supersonic reacting wall jet
3. Large-Eddy/Reynolds-Averaged Navier–Stokes Simulations of Reactive Flow in Dual-Mode Scramjet Combustor
4. Large-eddy/Reynolds-averaged Navier–Stokes simulation of cavity-stabilized ethylene combustion
5. Turbulence / Chemistry Interactions in a Ramp-Stabilized Supersonic Hydrogen-Air Diffusion Flame
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1. Multi-Resolution Analysis for Assessment of Subgrid Turbulence / Chemistry Interactions in Supersonic Combustion;AIAA SCITECH 2024 Forum;2024-01-04
2. Large Eddy Simulation and Dynamic Mode Decomposition of Supersonic Combustion Instability in a Strut-Based Scramjet Combustor;Aerospace;2023-09-29
3. Mesh-Sequenced Realizations for Evaluation of Subgrid-Scale Models for Turbulent Combustion;AIAA Journal;2020-11
4. Least Squares Minimization Closure Models for LES of Turbulent Combustion;Flow, Turbulence and Combustion;2018-08-07
5. Mesh-Sequenced Realizations for Evaluation of Subgrid-Scale Models for Turbulent Combustion;2018 AIAA Aerospace Sciences Meeting;2018-01-07
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