Vortical Dynamics and Acoustic Response in Gas-Turbine Swirl-Stabilized Injectors.
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American Institute of Aeronautics and Astronautics |
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The Effect of Fuel Injector Geometry on The Flow Structure of a Swirl Stabilized Gas Turbine Burner.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Prediction of acoustic pressure spectra in combustion systems using swirl stabilized gas turbine burners.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
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Spray and Emission Characteristics Near Lean Blow Out in a Counter-Swirl Stabilized Gas Turbine Combustor.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Effect of Swirl Injector Design and Other Important Parameters on Gas Turbine Combustion
American Institute of Aeronautics and Astronautics |
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Surface- Stabilized Fuel Injectors with Sub- Three PPM NOx Emissions for a 5.5 MW Gas Turbine Engine.
American Society of Mechanical Engineers |