Invited talks

  1. Dynamic stall and its prediction. (2024). Indian Institute of Technology Delhi; .
  2. Aerodynamic whistle-based ultrasonic bat deterrents. (2023). Renewable Energy Wildlife Institute (REWI); .
  3. Passive, blade-mounted ultrasonic bat deterrents. (2021). American Wind and Wildlife Institute; .
  4. Numerical investigations of quiet blade designs inspired by the unique feather features of the night owl. (2017). Indian Institute of Science; .
  5. Numerical investigations of quiet blade designs inspired by the unique feather features of the night owl. (2017). Indian Institute of Technology, Bombay; .
  6. Analysis and design of a novel conceptual turbine to enhance wind farm efficiency. (2017). Rensselaer Polytechnic Institute; .
  7. Innovative solutions to enhance wind turbine/farm performance and reduce noise. (2016). University of Kansas; .
  8. Wind turbine and wind farm aerodynamics and aeroacoustics. (2014). University of Illinois at Urbana Champaign; .
  9. Gas turbine cycle analysis with a focus on propulsion. (2014). General Electric Global Research Center; .
  10. Windfarm aerodynamics and aeroacoustics. (2013). Argonne National Laboratory; .
  11. Aerodynamic tone noise from open rotors. (2012). Indian Institute of Technology Delhi; .
  12. Aerodynamic tone noise from open rotors. (2012). NASA Langley Research Center; .
  13. An overview of GE’s research in aeroacoustics. (2010). The University of Cambridge; .
  14. Blast-impact simulations using direct simulation monte carlo, and turbomachinery aeroacoustics. (2006). Indian Institute of Technology Delhi; .
  15. Rotor-Stator Internation Tone Noise Prediction. (2006). NASA Glenn Research Center; .

Regular talks

  1. Numerical investigations of quiet blade designs inspired by the unique feather features of the night owl. (2018). US Naval Research Center; .
  2. Numerical investigations of quiet blade designs inspired by the unique feather features of the night owl. (2017). General Electric Aviation; .
  3. Effect of airfoil thickness on incipience of dynamic stall at Re=200,000. (2016). Air Force Research Laboratory; .
  4. Blast-impact simulations using direct simulation monte carlo, and turbomachinery aeroacoustics. (2006). Indian Institute of Technology Madras; .
  5. Parallel algorithms for particle methods for fluid flow. (2004). SIAM Conference for Parallel Computing; .