Computational Investigation of Combustion Instabilities in a Laboratory-Scale LDI Gas Turbine Engine
Author:
Affiliation:
1. Purdue University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3648
Reference23 articles.
1. Stability and Control of Lean Blowout in Chemical Kinetics-Controlled Combustion Systems
2. The dissipation of sound at an edge
3. Computational Investigation of Acoustics and Instabilities in a Longitudinal-Mode Rocket Combustor
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1. Combustion Dynamics in a Single-Element Lean Direct Injection Gas Turbine Combustor;Combustion Science and Technology;2019-07-31
2. Simulation of combustion characteristics in a hydrogen fuelled lean single-element direct injection combustor;International Journal of Hydrogen Energy;2017-02
3. 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
4. Combustion Dynamics Behavior in a Single-Element Lean Direct Injection (LDI) Gas Turbine Combustor;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
5. Computational Study of Combustion Dynamics in a Single-Element Lean Direct Injection Gas Turbine Combustor;52nd Aerospace Sciences Meeting;2014-01-10
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