Amit Kumar
Technical University of Denmark, Indian Institute of Technology Bombay, Aeronautical Society of India
About
Dr. Amit Kumar is a postdoctoral researcher at the Technical University of Denmark (DTU). He got his M.Tech. and Ph.D. from the Department of Aerospace Engineering, Indian Institute of Technology Bombay (IIT Bombay), India. He received the Young Engineer Turbo Expo Participation Travel Award from the American Society of Mechanical Engineers-International Gas Turbine Institute in 2021 and 2022. Based on his doctoral and postdoctoral research, he has contributed to 11 journals and 7 international conference papers on turbomachinery design and analysis, blending experimental and numerical investigations.
Primary areas of expertise are: • Aerodynamic design of turbomachinery blades • Computational Fluid Dynamics • Experimental techniques in turbomachinery • Multiphase-flow• Design of Turbomachinery for two-phase flow
Employment
-
Technical University of Denmark Postdoc2022 - 2024
-
Indian Institute of Technology Bombay Postdoc2021 - 2022
Education
-
Indian Institute of Technology Bombay PhD2016 - 2022
-
Indian Institute of Technology Bombay M. Tech2013 - 2015
-
Aeronautical Society of India Bachelor of Technology B2009 - 2013
Projects & Funding
Projects & funding information is unavailable.
Publications (21)
- Transient analysis of stall onset in highly-loaded tandem rotor configurations for an axial compressor Save
- Understanding the Effect of Three-Dimensional Design in Tandem Blade Save
- Aerodynamics of a Tandem-Bladed Axial Compressor Rotor under Circumferential Distortion at Different Rotational Speeds Save
- Numerical Investigation of Flashing Flow in a Convergent-Divergent Nozzle Save
- Preliminary Analysis of Two-Phase Expansion on Liquid Air Energy Storage System Integrated to a Conventional Pressurized Water Reactor Save
- Effects of Radial Distortion on Low-Speed Tandem Stage Axial Compressor Save
- Numerical Simulations on Performance of a Hybrid and a Tandem Rotor Save
- UNDERSTANDING THE EFFECT OF THREE-DIMENSIONAL DESIGN IN TANDEM BLADE Save
- Effect of Differential Tip Clearance on the Performance of a Tandem Rotor Save
- Spike type of stall inception in the tandem rotor Save