Combustion Dynamics of Rocket Engine and Its active control using high energy plasma discharge for Phase Desynchronization
Implementing Organization
Sardar Vallabhbhai National Institute Of Technology
Principal Investigator
Dr. Baraiya Nikhil Ashokbhai
Assistant Professor
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Sardar Vallabhbhai National Institute Of Technology
Mechanical Engineering
CO-Principal Investigator
Shri S K Nathan
Mahendragiri, Tamil Nadu
ISRO Propulsion Complex
Project Overview
The project is being executed in three phases. The first phase of the work includes stability mapping of the combustor across state variables like equivalence ratios, pressure, flow rates, etc. Across these operating conditions, the various dynamical states attained by the system will be analyzed using frequency spectra. The second phase includes using non-stationary time series analysis to identify critical dynamical states attained by the combustion system and explore the nature of the instability. The last phase of the work deals with the active control of the combustion instability using high-energy plasma discharge.
Sardar Vallabhbhai National Institute Of Technology
Assistant Professor
Mechanical Engineering
Acces sibility Controls