Dr Manish Kumar

Background:

• Research Associate in Gas Turbine Combustion System Aerothermal Technology
• Member of the Rolls-Royce UTC in Combustion System Aerothermal Processes since 2024.

Specialities:

• Experimental study of reacting flows within combustion systems and combustion system aerodynamics.
• Emissions measurements.
• Combustion characteristics measurement using chemiluminescence, thermocouple, high speed shadowgraphy, Spectrometer.

Research group:

Applied Aerodynamics and combustion.

Current research:

Experimental and computational fluid dynamics, reacting flows, Spray and Droplet, Swirl Combustion, Combustion system aerodynamics, IC Engine Combustion, Liquid Propellant, Gas Turbine and Rocket Engine, Advanced Propulsion Devices, Laser Diagnostic.

Teaching Assistant for Rocket Propulsion, Combustion, Gas turbine engine offered by Prof. Srinibas Karmakar at Indian Institute of Technology, Kharagpur

External activities:

• Member if the Rolls-Royce UTC in Combustion System Aerothermal Processes.
• Member of combustion institute (Israeli Section)