Research Engineer : Thermoacoustic Combustion Instabilities
I worked on advancing scientific and computational methods to address combustion instabilities, a critical challenge in designing gas turbines and liquid rocket engines. These instabilities arise from the complex interplay between flame dynamics and acoustics, and mitigating their effects requires deep technical insights. My work focused on two approaches:1. Instantaneous Modal Decomposition (IMD): - Developed and implemented IMD to reconstruct acoustic pressure and velocity fields in combustion chambers. - Applied IMD within the STORM (State-space Thermoacoustic low-ORder Model) framework to analyze transient regimes in complex 3D geometries, including the Hylon burner case. - Addressed limitations of IMD, such as its inability to capture non-acoustic pressure fluctuations, enhancing its robustness for real combustor scenarios. 2. Helmholtz-Hodge Decomposition (HHD): - Implemented HHD to decompose vector fields into vortical, compressible, and harmonic components, aiding in the localization and identification of noise sources. - Utilized the open-source FEM code FEniCS for solving PDEs and validating results using analytical functions. - Extended the method from 2D to complex 3D cases, successfully separating and comparing acoustic and vortical potentials. This work provides a solid foundation for improving thermoacoustic predictions and designing more stable combustion systems.