A new BML-based RANS modelling for the description of gas turbine typical combustion processes
Author:
Publisher
Inderscience Publishers
Subject
Computer Science Applications,Condensed Matter Physics
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. Wall temperature considerations in a two-stage swirl non-premixed furnace;Progress in Computational Fluid Dynamics, An International Journal;2014
2. Toward the Impact of Fuel Evaporation-Combustion Interaction on Spray Combustion in Gas Turbine Combustion Chambers. Part I: Effect of Partial Fuel Vaporization on Spray Combustion;ERCOFTAC Series;2011
3. 3D RANS Simulation of Turbulent Flow and Combustion in a 5 MW Reverse-Flow Type Gas Turbine Combustor;Journal of Engineering for Gas Turbines and Power;2010-08-11
4. Study on the potential of BML-approach and G-equation concept-based models for predicting swirling partially premixed combustion systems: URANS computations;Combustion and Flame;2008-03
5. Modeling and 3D-Simulation of the Kinetic Effects in the Post-Flame Region of Turbulent Premixed Flames Based on the G-Equation Approach;Flow, Turbulence and Combustion;2005-12
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