Cost-constrained adaptive simulations of transient spray combustion in a gas turbine combustor-Reference-Cited by-同舟云学术

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Cost-constrained adaptive simulations of transient spray combustion in a gas turbine combustor

Published:2023-03 Issue: Volume:249 Page:112530
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Mohaddes Danyal^ORCID,Brouzet Davy,Ihme Matthias^ORCID

Funder

Boeing

National Aeronautics and Space Administration

Office of Science

Naval Air Systems Command

National Energy Research Scientific Computing Center

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference59 articles.

1. A physics-based approach to modeling real-fuel combustion chemistry—I. Evidence from experiments, and thermodynamic, chemical kinetic and statistical considerations;Wang;Combust. Flame,2018

2. Fuel effects on lean blow-out in a realistic gas turbine combustor;Esclapez;Combust. Flame,2017

3. Analysis of low-temperature chemistry in a turbulent swirling spray flame near lean blow-out;Mohaddes;Proc. Combust. Inst.,2021

4. Analysis of segregation and bifurcation in turbulent spray flames: a 3D counterflow configuration;Vié;Proc. Combust. Inst.,2015

5. Large-eddy simulations of transcritical injection and auto-ignition using diffuse-interface method and finite-rate chemistry;Ma;Proc. Combust. Inst.,2019

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis of direct and indirect noise in a next-generation aviation gas turbine combustor;Combustion and Flame;2024-02

2. Coupling of detonation structure and upstream inhomogeneities in a rotating detonation engine;Proceedings of the Combustion Institute;2024

3. Augmenting filtered flame front displacement models for LES using machine learning with a posteriori simulations;Proceedings of the Combustion Institute;2024

4. On the noise analysis of a N+3 next-generation combustor through LES;AIAA AVIATION 2023 Forum;2023-06-08

5. Adaptive Modeling of Supersonic Combustion in a Cavity-Stabilized Scramjet;AIAA SCITECH 2023 Forum;2023-01-19

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