NK
Naveen Kumar
National Tsing Hua University, Indian Institute of Technology Dharwad, Indian Institute of Technology Roorkee, Dr. A.P.J. Abdul Kalam Technical University, Indian Institute of Technology Kanpur
About
After completing PhD from IIT Roorkee in July 2023, I worked as a Post-doctoral Fellow at IIT Kanpur from August-November 2023. Currently working as post-doctoral researcher at IIT Dharwad since December 2023. I am engaged in full-scale 3D simulations of hypersonic nozzles and space vehicles using Large Eddy Simulation (LES) and hybrid Detached Eddy Simulation (DES) methods.
Employment
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National Tsing Hua University Postdoctoral Research Fellow2026 - 2026
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Indian Institute of Technology Dharwad Institute Post-Doctoral Fellow (I-PDF)2023 - 2026
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Indian Institute of Technology Kanpur Post-Doctoral Fellow (PDF)2023 - 2023
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Indian Institute of Technology Roorkee Research Scholar2017 - 2023
Education
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Indian Institute of Technology Roorkee PhD2017 - 2023
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Dr. A.P.J. Abdul Kalam Technical University B.Tech2004 - 2008
Projects & Funding
Projects & funding information is unavailable.
Publications (17)
- Comparative assessment of Eddy-Dissipation Concept (EDC) models for turbulence-chemistry interaction in hypersonic flow over a Mars entry vehicle Save
- NUMERICAL INVESTIGATION OF SHOCK LAYER BEHAVIOR IN SPACE VEHICLES AT VARYING MACH NUMBERS USING OpenFOAM Save
- Effect of turbulence on flow and heat transfer in high-area-ratio (HAR) rocket nozzles Save
- Development of Immersed Boundary Method for High-Speed Compressible Flows in OpenFOAM Save
- Flow modelling of a rocket nozzle using hydrogen and methane propellants Save
- Effects of Turbulence-Chemistry Interactions (TCI) on Flow-Fields of a Martian Space Vehicle Save
- Numerical Comparison of Turbulence-Chemistry Interactions Models with Radiation Effect for Non-Premixed Flames: Sandia-E and DLR-B Save
- Combustion and Radiation Modeling of Non-premixed Turbulent DLR-A Flame Save
- Analysing Convective Heat Transfer Over a Blunt Cone Across Different Gas Environments Save
- Modeling of turbulence, chemistry, and heat transfer of a rocket nozzle Save