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The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor. [PDF]
Gövert S +4 more
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Discrete imaging models for three-dimensional optoacoustic tomography using radially symmetric expansion functions. [PDF]
Wang K +4 more
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Perspectives on NO X Emissions and Impacts from Ammonia Combustion Processes. [PDF]
Mashruk S +15 more
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Nonlinear natural engine: Model for thermodynamic processes in mesoscale systems. [PDF]
Wheatley J +4 more
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Commentary: an eye on PET quantification. [PDF]
Walker MD, Sossi V.
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Condensed Matter Systems Exposed to Radiation: Multiscale Theory, Simulations, and Experiment. [PDF]
Solov'yov AV +22 more
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SENSITIVITY ANALYSIS OF THERMOACOUSTIC INSTABILITIES
24th International Conference on Sound and Vibration 2017, London CallingThermoacoustic instability is a phenomenon that occurs in numerous combustion systems, from rockets to land-based gas turbines. The thermoacoustic oscillations of these systems are of significant importance as they can result in severe vibrations, thrust
F SOGARO, P SCHMID, AS MORGANS
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Intrinsic thermoacoustic instabilities
Progress in Energy and Combustion Science, 2023Camilo F. Silva
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The Physics of Fluids, 2022
The present study investigates the effect of exit geometry of the main stage in a model combustor with a dual-swirl layout. In practical combustors, the main stage has much larger airflow than the pilot stage, therefore dominating the aerodynamics of the
Meng Han +3 more
semanticscholar +1 more source
The present study investigates the effect of exit geometry of the main stage in a model combustor with a dual-swirl layout. In practical combustors, the main stage has much larger airflow than the pilot stage, therefore dominating the aerodynamics of the
Meng Han +3 more
semanticscholar +1 more source

