|
Projects |
Sponsored Projects:
|
Sl. No. |
Sponsoring Agency |
Project Title |
Duration |
|
1. |
Aeronautics Research and
Development Board, Propulsion Panel |
Active
boundary layer control in 2-D cascade and axial flow fan |
2006-2008 |
|
2. |
Aeronautics Research and
Development Board, Propulsion Panel |
Axial
fan performance evaluation and enhancement strategies under static and
dynamic inflow distortions |
2008-2010 |
|
3. |
Siemens Energy Inc., Florida,
USA |
Annular turbine diffuser
aerodynamics (Co-investigator: Prof. Bhaskar
Roy) |
2008-2013 |
|
4. |
Pratt and Whitney, Canada |
Tip Flow in High Hub-tip Ratio
Axial Flow Compressors (Co-investigator: Prof. Bhaskar
Roy) |
2009-2012 |
|
5. |
Aeronautics Research and
Development Board, Propulsion Panel |
Parametric study of
contra-rotating axial flow fans under different inflow conditions and design
modifications based on the parametric study (Co-investigator: Prof.
Bhaskar Roy) |
2012-2014 |
|
6. |
Aeronautical Development Agency |
Flow characteristics, active
and passive flow control in a serpentine intake duct |
2011-2014 |
|
7. |
Aeronautics Research and
Development Board, Aerodynamics Panel |
Investigation of secondary flow
and its control in an axial compressor cascade with and without tip gap (Co-investigator: Prof. Bhaskar
Roy) |
2013-2015 |
|
8. |
Defence Research and
Development Organization |
Effect of inflow distortion on
fan performance |
2017-2020 |
|
9. |
Defence Research and
Development Organization |
Losses in a fan-booster duct |
2017-2020 |
|
10. |
Defence Research and
Development Organization |
Design and analysis of a mixed
flow compressor |
2017-2020 |
|
11. |
Gas Turbine Research
Establishment, DRDO |
Axial turbine performance
characterization (Co-Investigator: Prof. T
Chandra Sekar) |
2023-2024 |
|
12. |
Gas Turbine Research
Establishment, DRDO |
3D radial stacking in
multi-stage axial compressors (Co-Investigator: Prof. T
Chandra Sekar) |
2023-2025 |
|
13. |
Aeronautics Research and
Development Board, Propulsion Panel |
Experimental investigation and
optimization of turbine 3D nozzle guide vanes (Principal investigator: Prof.
T Chandra Sekar) |
2023-2025 |
|
14. |
SERB, India |
Surface roughness effects in
axial compressors (Co-Investigator: Prof. T
Chandra Sekar) |
2024-2026 |
|
15. |
Honeywell Aerospace, India |
Total pressure loss of stator
vanes without and with injection (Co-Investigator: Prof. T
Chandra Sekar) |
2025-2026 |
Consultancy Projects:
Consultancy
projects from several agencies like, ADE Bangalore, DARE Bangalore, Nostrum
Technologies Pvt Ltd Mumbai, Sudha Ventillators
Ahmednagar,
Technoforce Solutions Nashik, Tata Power Mumbai, Archeological Survey of India (Ministry of Culture),
L&T Defense etc.