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

Implementing Organization

Indian Institue of Technology (IIT) Jammu, Jammu and Kashmir
Principal Investigator
Dr. Shanmugadas K P
Assistant Professor
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Indian Institue of Technology (IIT) Jammu, Jammu and Kashmir
Dept. of Mechanical Engineering
CO-Principal Investigator
Shri Ganesh P
Mahendragiri, Tamil Nadu
ISRO Propulsion Complex (IPRC), ISRO

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.

Related Research

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Funding Organization
Funding Organization
Department of Space (DoS)
Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Propulsion- Testing of high thrust liquid rocket engines
Start Year
2024
Sanction Amount
₹ 24.58 L
Status
Ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
N/A
Startup (If Any)
00
No. of Patents
Filed :00
Grant :00
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