Large eddy simulation with flamelet progress variable approach combined with artificial neural network acceleration
Author:
Affiliation:
1. King Abdullah University of Science and Technology
2. University of Rome "La Sapienza"
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Progress-variable approach for large-eddy simulation of non-premixed turbulent combustion
2. Deep Residual Networks for Flamelet/progress Variable Tabulation with Application to a Piloted Flame with Inhomogeneous Inlet
3. Application of deep artificial neural networks to multi-dimensional flamelet libraries and spray flames
4. Implementation of high dimensional flamelet manifolds for supersonic combustion using deep neural networks
5. Effects of turbulence on species mass fractions in methane/air jet flames
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