Data driven techniques applied to numerical and experimental study of jet in cross flow
Implementing Organization
Indian Institute of Technology (IIT)
Principal Investigator
Prof. Arnab Roy
Indian Institute Of Technology (IIT) Kharagpur, West Bengal
CO-Principal Investigator
Prof. Parthasarathi Ghosh
Indian Institute of Technology (IIT)
About
Jet in cross flow is a complex problem with numerous applications in aerospace and other engineering disciplines. It involves various flow physics, including jet velocity ratio, jet orifice geometry, compressibility, single and multiphase flow, steady and pulsating jet, particulate laden jet, and more. The research proposal aims to use data-driven techniques to analyze the jet cross flow interaction, obtaining better understanding of spatio-temporal dynamics, optimizing practical configurations, and developing reduced order models for real-time control. The study will involve physical experiments and numerical computations, with two components: a compressed air jet deployed in a supersonic wind tunnel test section, and a seeded water jet in a water tank. The jet assembly will be mounted on a traverse and followed by a high-speed camera. Velocity field will be obtained using Particle Image Velocimetry. Numerical simulations of the flow problems will be performed using eddy resolving simulations of the Navier Stokes equations, and the PI has extensive experience in applying modal decomposition of unsteady flow fields using Proper Orthogonal Decomposition (POD). Dynamic Mode Decomposition (DMD) will be used to extract dynamically dominant modes, their growth/decay, and associated frequencies. Several state-of-the-art data-driven techniques will also be used in the study. This research aims to provide a better understanding of jet cross flow interactions, optimize practical configurations, and develop reduced order models for real-time control in aerospace applications.
Source
Source
Anusandhan National Research Foundation/Science and Engineering Research Board (SERB), DST 2023-24
Science and Engineering Research Board (SERB), New Delhi
Anusandhan National Research Foundation (ANRF)
Quick Information
Area of Research
Engineering Sciences
Start Year
2023
End Year
2026
Sanction Amount
₹ 50.07 L
Status
Ongoing
Contact
arnab@aero.iitkgp.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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