Large-Eddy Simulation of a High-Pressure, Single-Element Lean Direct-Injected Gas-Turbine Combustor
Author:
Affiliation:
1. Georgia Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0131
Reference20 articles.
1. The Structure of a Swirl-Stabilized Reacting Spray Issued from an Axial Swirler
2. Investigation of Swirling Air Flows Generated by Axial Swirlers in a Flame Tube
3. Flame Stabilization Modes in Lean Premixed Swirl Stabilized Combustion
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1. Affordable Explicitly Filtered Large-Eddy Simulation for Reacting Flows;AIAA Journal;2019-02
2. A Multifidelity Approach to Parameter Dependent Modeling of Combustion Instability;2018 Joint Propulsion Conference;2018-07-08
3. Experimental Investigation of Spray and Combustion Performances of a Fuel-Staged Low Emission Combustor: Effects of Main Swirl Angle;Journal of Engineering for Gas Turbines and Power;2017-08-23
4. Effects of Physical Modeling on Combustion Instability Predictions in a Single-Element Lean Direct Injection Gas Turbine Combustor;53rd AIAA Aerospace Sciences Meeting;2015-01-02
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