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Dr. Rinku Mukherjee

Associate Professor
Aerodynamics and Flow-Physics Laboratory
Applied Mechanics and BioMedical Engineering
Indian Institute of Technology Madras
Chennai, Tamil Nadu, India - 600036

Lab News & Updates

Jan 2025
Three papers from our lab were presented at AIAA SciTech 2025 in Orlando, Florida by
Hariprasanth Palanivel (AIAA 2025-0841),
Dr. Rinku Mukherjee (AIAA 2025-1076),
Shiladitya Bhowmick (AIAA 2025-0254).
Nov 2024
Dr. Rinku Mukherjee gave an invited talk in the 4th International Forum on Aerospace and Aeronautics and Physics and Astonomy Budapest, Hungary, Nov 2024.
Nov 2024
Vasanth Kumar's Journal paper published in Fluid Dynamics.
Oct 2024
Hariprasanth Palanivel's Journal paper published in Acta Mechanica.
Jul 2024
PhD scholar, Egambaravel J graduated.

Show and Tell

Research Areas: Numerical Analysis, CFD, Experiment

  Applied Aerodynamics

  • Unsteady Aerodynamics of Fixed-Wings
  • Post-Stall Flow Prediction (Steady & Unsteady)
  • Formation Flight
  • Experiments to Implement Post-Stall Flow Control
  • Wing in ground effect

    CFD Animation of Single Pitching Airfoil

    CFD Animation of Tandem Pitching Airfoils

    Flow past Single Airfoil in Water Tank

    Flow past Tandem Airfoils in Water Tank

    Wake behind a Pitching 3D Wing from Numerical Analysis

  Low-Speed Aerodynamics

  • Diamond-Back Morphing Wing with/without slender fuselage
  • Rectangular Wing with Airfoil-Shaped Vortex Generators

    Oil Flow Visualization of Flow Past a Wing

  High-Speed Aerodynamics

  • Diamond-Back Morphing Wing with/without slender fuselage at transonic and supersonic flows
  • Transonic Flows past Bluff-Bodies
  • Interaction of Boundary Layers and Shock Waves

    Transonic Flow Past a NASA specified Bluff Body

    Transonic Flow Past a Bluff Body with 20deg nose cone without Spike

    Transonic Flow Past a Bluff Body with 20deg nose cone WITH Spike

  Fundamental Fluid Mechanics

  • Boundary Layer Separation (2D and 3D) over wings and Bluff Bodies
  • Rayleigh-Benard Convection in Jet-A Fuel

Intellectual Property (IP) Generated

Copyrights Granted

Patent(s)