Experimental characterization and Parametric study on liquid jet penetration and break-up in a free supersonic gas jet

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Implementing Organization

Indian Institue of Technology (IIT) Jammu, Jammu and Kashmir

Principal Investigator

Dr. Shanmugadas K P

Assistant Professor, Dept. of Mechanical Engineering, Indian Institue of Technology (IIT) Jammu, Jammu and Kashmir

CO-Principal Investigator

Shri Ganesh P

ISRO Propulsion Complex (IPRC), ISRO, Mahendragiri, Tamil Nadu

Project Overview

The project aims to investigate the jet in cross flow atomization process using different non-intrusive flow diagnostic techniques. The existing jet in cross flow test facility will be modified to a free supersonic test facility with an injector traverse arrangement. Experiments will be conducted at M=3 operating conditions, and at scaled-down flow conditions as per IPRC requirements. Five injector configurations will be tested with and without swirl arrangement.

Achievements

The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society.

Source

Indian Space Research Organisation (ISRO)- Department of Space (DOS) 2022-2089

Related Research

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Quick Information

Area of Research

Astronomy & Space Sciences

Focus Area

Propulsion- Testing of high thrust liquid rocket engines

Start Date

2024

Status

ongoing

Contact

shanmugadas.kp@iitjammu.ac.in

Output

No. of Research Paper

Technologies (If Any)

No. of PhD Produced

Publications

No. of Patents

Filed : 00

Grant : 00

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