Awards and Recognition
First prize in the student poster competition at the ASME Gas Turbine India 2023 Conference (ASME GTIndia, 2023)
Conferences/Presentation
Krishna Chaitan Marthi and Santanu De, Development of a Transported FDF solver within LES framework, HPC Symposium 2024 (POSTER)
Krishna Chaitan Marthi, LES-of PRECCINSTA gas turbine combustor using Eulerian Stochastic Fields method, Research Scholar Day 2024. (Talk)
Krishna Chaitan Marthi, Santanu De, Large Eddy Simulation of a Partially-Premixed Swirl-Stabilized Combustor Using Transported Filtered Density Function Approach, ASME Gas Turbine India 2023 Conference (POSTER)
Anuj Kumar, Krishna Chaitan Marthi, Eshan Sharma and Santanu De, Numerical investigation of differential diffusion in a laminar, H2/N2 diffusion flame, 6th SEEC conference 2021 (ORAL)
Ongoing Research:
Fig: Contour of temperature, mixture fraction and axial velocity (left) unstable case, (right) stable case using LES-ESF approach
Fig: Contour of axial velocity for cold flow simulations of PRECCINSTA combustor using LES-ESF approach
POSTER PRESENTATION
Development of large eddy simulations of reactive flow using Eulerian stochastic field method coupled with tabulated chemistry. A solver named HybridESFFoam is currently developed. It is currently validated against Sandia Flame series.
Large Eddy Simulations of turbulent piloted methane jet flame Sandia DÂ & F using transported filtered density function (FDF) for turbulence-chemistry interaction. The transported FDF is solved stochastically using the Eulerian stochastic field method. The contour of temperature for both Flame D and F is shown below. A solver named ESFFoam has been developed.
Figure: Instantaneous snapshots of Temperature for Flame D (left) and Flame F (right)
From the above contours we can observe local extinction is observed for Flame F and almost no extinction is observed for Flame D. Low extinction is observed near the jet entrance for both Flame D and Flame F because of the stabilization provided by the pilot gas.
From the above contours we can observe local extinction is observed for Flame F and almost no extinction is observed for Flame D. Low extinction is observed near the jet entrance for both Flame D and Flame F because of the stabilization provided by the pilot gas.