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
|
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
About
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
Source
Indian Space Research Organisation (ISRO)- Department of Space (DOS) 2022-2089
Propulsion- Testing of high thrust liquid rocket engines
Start Year
2024
Sanction Amount
₹ 24.58 L
Status
completed
Contact
shanmugadas.kp@iitjammu.ac.in
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
No. of Patents
Filed :00
Grant :00
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